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CDAWeb Served Heliophysics Datasets

A1_K0_MPA: LANL 2001 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
A2_K0_MPA: LANL 2002 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
AC_AT_DEF: ACE Hourly RTN, GSE and J2000 GCI Attitude direction cosines - E. C. Stone (California Institute of Technology)
AC_H0_MFI: H0 - ACE Magnetic Field 16-Second Level 2 Data - N. Ness (Bartol Research Institute)
AC_H0_SWE: ACE/SWEPAM Solar Wind Experiment 64-Second Level 2 Data - D. J. McComas (SWRI)
AC_H1_EPM: ACE/EPAM Solar Energetic Particle 5-minute Level 2 Data - R. Gold (JHU/APL)
AC_H1_MFI: H1 - ACE Magnetic Field 4-Minute Level 2 Data - N. Ness (Bartol Research Institute)
AC_H1_SIS: ACE/SIS Solar Isotope Spectrometer 256-sec Level 2 Data - E. C. Stone (California Institute of Technology)
AC_H2_CRIS: ACE/CRIS Cosmic Ray Isotope Spectrometer 1-Hour Level 2 Data - E. C. Stone (California Institute of Technology)
AC_H2_EPM: ACE/EPAM Solar Energetic Particle 1-Hour Level 2 Data - R. Gold (JHU/APL)
AC_H2_MFI: H2 - ACE Magnetic Field 1-Hour Level 2 Data - N. Ness (Bartol Research Institute)
AC_H2_SEP: ACE/SEPICA Solar Energetic Particle 1-Hour Level 2 Data - Eberhard Moebius (University of New Hampshire)
AC_H2_SIS: ACE/SIS Solar Isotope Spectrometer 1-Hour Level 2 Data - E. C. Stone (California Institute of Technology)
AC_H2_SWE: ACE/SWEPAM Solar Wind Experiment 1-Hour Level 2 Data - D. J. McComas (SWRI)
AC_H2_SWI: ACE/SWICS 1.1 Solar Wind 1-Hour Level 2 Data - G. Gloeckler (University of Maryland)
AC_H2_ULE: ACE/ULEIS Solar Energetic Particle 1-Hour Level 2 Data - G. Mason (JHU/Applied Physics Lab)
AC_H3_CRIS: ACE/CRIS Cosmic Ray Isotope Spectrometer Daily-averaged Level 2 Data - E. C. Stone (California Institute of Technology)
AC_H3_EPM: ACE/EPAM Solar Energetic Particle 12-second Level 2 Data - R. Gold (JHU/APL)
AC_H3_MFI: H3 - ACE Magnetic Field 1-Second Level 2 Data - N. Ness (Bartol Research Institute)
AC_H3_SW2: ACE/SWICS 2.0 Solar Wind 2-Hour Level 2 Data - G. Gloeckler (University of Maryland)
AC_H3_SWI: ACE/SWICS 1.1 Solar Wind 2-Hour Level 2 Data - G. Gloeckler (University of Maryland)
AC_H4_SWI: ACE/SWICS 1.1 Solar Wind 1-Day Level 2 Data - G. Gloeckler (University of Maryland)
AC_H5_SWI: ACE/SWICS 1.1 Solar Wind 2-Hour Level 2 Q-state distributions - G. Gloeckler (University of Maryland)
AC_H6_SWI: ACE/SWICS Solar Wind Protons 12-min Level 2 Data - G. Gloeckler (University of Maryland)
AC_K0_EPM: K0 - ACE EPAM 5-Minute Key Parameters - R. Gold (JHU Applied Physics Laboratory)
AC_K0_GIFWALK: Links to ACE KP pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
AC_K0_MFI: K0 - ACE Magnetic Field 5-Minute Key Parameters - N. Ness (Bartol Research Institute)
AC_K0_SIS: K0 - ACE SIS 1-Hour Key Parameters - E. C. Stone (California Institute of Technology)
AC_K0_SWE: K0 - ACE Solar Wind Experiment 5-Minute Key Parameters - D. J. McComas (NASA LANL)
AC_K1_EPM: K1 - ACE EPAM 1-Hour Key Parameters - R. Gold (JHU Applied Physics Laboratory)
AC_K1_MFI: K1 - ACE Magnetic Field 16-Second Key Parameters - N. Ness (Bartol Research Institute)
AC_K1_SWE: K1 - ACE Solar Wind Experiment 1-Hour Key Parameters - D. J. McComas (NASA LANL)
AC_K2_MFI: K2 - ACE Magnetic Field 1-Hour Key Parameters - N. Ness (Bartol Research Institute)
AC_OR_DEF: ACE Daily GSE and J2000 GCI Position Data - E. C. Stone (California Institute of Technology)
AC_OR_SSC: ACE GSE Positions @ 12 min resolution - SSC/SSCWeb ( NASA's GSFC)
AEROCUBE-6-A_DOSIMETER_L2: Aerocube 6/Dosimeter Level 2 - J. B. Blake (The Aerospace Corporation)
AEROCUBE-6-B_DOSIMETER_L2: Aerocube 6/Dosimeter Level 2 - J. B. Blake (The Aerospace Corporation)
AIM_CIPS_SCI_3A: AIM Cloud Imaging and Particle Size (CIPS) Polar Mesospheric Clouds (PMC) Daily Images - Cora E. Randall (University of Colorado)
ALOUETTE2_AV_LIM: ALOUETTE Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
ALOUETTE2_AV_QUI: ALOUETTE Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
ALOUETTE2_AV_SNT: ALOUETTE Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
ALOUETTE2_AV_SOL: ALOUETTE Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
ALOUETTE2_AV_ULA: ISIS-1 Topside Sounder Ionogram over Fairbanks, Alaska (lat/lon=65/212) - R.F. Benson (NASA GSFC)
ALOUETTE2_AV_WNK: ALOUETTE Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
ALOUETTE2_NEPROF_TOPS: ALOUETTE-2 CRC Electron Density Profiles - J. E. Jackson (Communication Research Centre (CRC), Ottawa)
AMPTECCE_H0_MEPA: AMPTE CCE MEPA High Time Resolution Energetic Particles - D. McEntire (JHU/APL)
APOLLO12_SWS_1HR: Apollo 12 Solar Wind measurements at the lunar surface - Conway W. Snyder (Jet Propulsion Laboratory )
APOLLO12_SWS_28S: Apollo 12 Solar Wind measurements at the lunar surface - Conway W. Snyder (Jet Propulsion Laboratory )
APOLLO15_SWS_1HR: Apollo 15 Solar Wind measurements at the lunar surface - Conway W. Snyder (Jet Propulsion Laboratory )
APOLLO15_SWS_28S: Apollo 15 Solar Wind measurements at the lunar surface - Conway W. Snyder (Jet Propulsion Laboratory )
AWE_L3A_TMP: Atmospheric Waves Experiment (AWE) on the ISS - Mesospheric Temperature Mapper - Swaths - Ludger Scherliess (Utah State University)
AWE_L3C_Q20: Atmospheric Waves Experiment (AWE) on the ISS - Mesospheric Temperature Mapper - Swaths - Q line Radiance - Ludger Scherliess (Utah State University)
BAR_1A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1A_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1B_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1B_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1B_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1B_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1B_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1B_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1B_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1C_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1C_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1C_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1C_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1C_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1C_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1C_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1D_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1D_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1D_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1D_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1D_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1D_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1D_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1G_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1G_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1G_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1G_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1G_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1G_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1G_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1H_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1H_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1H_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1H_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1H_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1H_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1H_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1I_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1I_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1I_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1I_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1I_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1I_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1I_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1J_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1J_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1J_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1J_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1J_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1J_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1J_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1K_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1K_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1K_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1K_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1K_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1K_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1K_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1M_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1M_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1M_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1M_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1M_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1M_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1M_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1N_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1N_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1N_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1N_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1N_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1N_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1N_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1O_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1O_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1O_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1O_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1O_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1O_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1O_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1Q_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1Q_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1Q_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1Q_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1Q_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1Q_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1Q_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1R_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1R_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1R_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1R_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1R_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1R_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1R_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1S_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1S_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1S_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1S_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1S_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1S_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1S_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1T_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1T_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1T_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1T_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1T_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1T_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1T_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1U_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1U_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1U_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1U_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1U_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1U_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1U_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1V_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_1V_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1V_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_1V_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_1V_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_1V_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_1V_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2A_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2B_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2B_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2B_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2B_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2B_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2B_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2B_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2C_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2C_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2C_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2C_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2C_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2C_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2C_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2D_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2D_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2D_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2D_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2D_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2D_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2D_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2E_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2E_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2E_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2E_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2E_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2E_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2E_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2F_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2F_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2F_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2F_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2F_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2F_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2F_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2I_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2I_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2I_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2I_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2I_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2I_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2I_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2K_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2K_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2K_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2K_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2K_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2K_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2K_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2L_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2L_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2L_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2L_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2L_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2L_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2L_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2M_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2M_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2M_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2M_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2M_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2M_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2M_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2N_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2N_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2N_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2N_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2N_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2N_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2N_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2O_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2O_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2O_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2O_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2O_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2O_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2O_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2P_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2P_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2P_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2P_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2P_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2P_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2P_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Q_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2Q_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Q_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2Q_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2Q_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Q_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2Q_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2T_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2T_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2T_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2T_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2T_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2T_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2T_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2W_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2W_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2W_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2W_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2W_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2W_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2W_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2X_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2X_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2X_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2X_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2X_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2X_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2X_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Y_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_2Y_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Y_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_2Y_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_2Y_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_2Y_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_2Y_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3A_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3B_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3B_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3B_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3B_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3B_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3B_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3B_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3C_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3C_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3C_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3C_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3C_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3C_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3C_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3D_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3D_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3D_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3D_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3D_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3D_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3D_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3E_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3E_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3E_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3E_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3E_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3E_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3E_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3F_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3F_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3F_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3F_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3F_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3F_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3F_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3G_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_3G_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3G_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_3G_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_3G_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_3G_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_3G_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4A_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4A_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4B_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4B_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4B_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4B_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4B_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4B_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4B_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4B_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4C_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4C_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4C_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4C_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4C_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4C_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4C_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4C_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4D_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4D_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4D_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4D_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4D_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4D_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4D_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4D_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4E_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4E_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4E_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4E_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4E_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4E_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4E_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4E_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4F_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4F_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4F_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4F_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4F_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4F_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4F_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4F_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4G_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4G_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4G_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4G_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4G_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4G_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4G_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4G_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_4H_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_4H_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4H_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_4H_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4H_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_4H_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_4H_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_4H_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_5A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_5A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_5A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_5A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_5A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_5A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_5A_L2_USPC: 10ms resolution x-ray spectra - Robyn Millan (Dartmouth College)
BAR_5A_L2_XSPC: 50ms resolution, 30-channel X-ray spectrum - Robyn Millan (Dartmouth College)
BAR_6A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_6A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_6A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_6A_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_6A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_6A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_6A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_7A_L2_EPHM: Coordinates - Robyn Millan (Dartmouth College)
BAR_7A_L2_FSPC: BARREL Fast Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_7A_L2_HKPG: Analog Housekeeping Data - Robyn Millan (Dartmouth College)
BAR_7A_L2_MAGN: MAG X, Y, and Z - Robyn Millan (Dartmouth College)
BAR_7A_L2_MSPC: BARREL Medium Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BAR_7A_L2_RCNT: Rate counters for scintillator diagnostics. - Robyn Millan (Dartmouth College)
BAR_7A_L2_SSPC: BARREL Slow Time Resolution Bremsstrahlung X-ray Spectra - Robyn Millan (Dartmouth College)
BEPICOLOMBO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
BEPICOLOMBO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
BIOSENTINEL_LET_LETS: The spacecraft is in earth-trailing heliocentric orbit and carries a Linear Energy Transfer Spectrometer LETS to capture energetic particle dose rates. - Sergio Santa Maria, Stuart George (NASA)
BORRELLY_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
BORRELLY_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
C1_CP_CIS-CODIF_H1_1D_PEF: This dataset contains CIS-CODIF Proton omni-directional distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HE1_1D_PEF: This dataset contains CIS-CODIF Helium+ omni-directional distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_H1_PEF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_H1_PF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_H1_PSD: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_HE1_PF: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_HE1_PSD: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_O1_PEF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_O1_PF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_HS_O1_PSD: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_O1_1D_PEF: This dataset contains CIS-CODIF Oxygen+ omni-directional distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_PAD_HS_H1_PF: This dataset contains CIS-CODIF Proton Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_PAD_HS_HE1_PF: This dataset contains CIS-CODIF Helium+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C1_CP_CIS-CODIF_PAD_HS_O1_PF: This dataset contains CIS-CODIF Oxygen+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_1D_PEF: This dataset contains CIS-HIA Ion omni-directional distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_MAG_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_MAG_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_MAG_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_SW_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_SW_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_HS_SW_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_LS_1D_PEF: This dataset contains Ion omni-directional fluxes in Particle_Energy_Flux units - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_LS_SW_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_LS_SW_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_LS_SW_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C1_CP_CIS-HIA_PAD_HS_MAG_IONS_PF: This dataset contains CIS-HIA Ion Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C1_CP_EDI_AEDC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C1_CP_EDI_MP: This dataset contains mixed (i.e. quarter- half- and one spin) resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C1_CP_EDI_QZC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C1_CP_EDI_SPIN: This dataset contains spin resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C1_CP_EFW_L3_E3D_INERT: This dataset contains 4-sec averages of the 3-dimensional Electric field vector - Mats Andre (IRFU)
C1_CP_EFW_L3_P: This dataset contains measurements of the - Yuri Khotyaintsev (IRFU)
C1_CP_EFW_L3_V3D_INERT: This dataset contains 4-sec averages of the ExB-drift velocity in ISR2, using - Mats Andre (IRFU)
C1_CP_FGM_5VPS: This dataset contains 5 vectors/second resolution measurements of the magnetic field vector from the FGM - Chris Carr (Imperial College)
C1_CP_FGM_SPIN: Cluster Spacecraft 1 FluxGate Magnetometer (FGM) Spin-Resolution Parameters
C1_CP_RAP_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C1_CP_RAP_ESPCT6: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C1_CP_RAP_HSPCT: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C1_CP_RAP_I3DM_CNO: This dataset contains differential fluxes of CNO - Berend Wilken (MPS)
C1_CP_RAP_I3DM_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C1_CP_RAP_I3DM_HE: This dataset contains differential fluxes of Helium - Berend Wilken (MPS)
C1_CP_RAP_ISPCT_CNO: This dataset contains differential fluxes of CNO - Berend Wilken (MPS)
C1_CP_RAP_ISPCT_HE: This dataset contains differential fluxes of Helium - Berend Wilken (MPS)
C1_CP_RAP_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C1_CP_RAP_PAD_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C1_CP_RAP_PAD_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C1_CP_RAP_PAD_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C1_CP_RAP_PAD_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C1_CP_RAP_PAD_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C1_CP_STA_CWF_GSE: This dataset contains measurements of the magnetic field - Patrick Canu (LPP)
C1_CP_STA_PPP: Polarization and propagation parameters - Patrick Canu (LPP)
C1_CP_STA_PSD: Power Spectral Density measurements of three - Patrick Canu (LPP)
C1_CP_STA_SM: Cross spectral matrices formed from - Patrick Canu (LPP)
C1_CP_WHI_ACTIVE: This dataset contains electric spectral power density under Sounding Mode from Whisper on spacecraft 1 - Pierre Henri (LPC2E)
C1_CP_WHI_ELECTRON_DENSITY: This dataset contains plasma frequencies from Whisper on spacecraft 1 - Pierre Henri (LPC2E)
C1_CP_WHI_NATURAL: This dataset contains electric spectral power density under natural mode from Whisper on spacecraft 1 - Pierre Henri (LPC2E)
C1_CP_WHI_PASSIVE_ACTIVE: This dataset contains passive electric spectral power density under sounding mode from Whisper on spacecraft 1 - Pierre Henri (LPC2E)
C1_CP_WHI_WAVE_FORM_ENERGY: This dataset contains the Electric Wave Form Power Density under natural mode from Whisper on spacecraft 1 - Pierre Henri (LPC2E)
C1_JP_PMP: Cluster Spacecraft 1, JSOC Predicted Magnetic Positions - (Non-PI) M. Hapgood (RAL)
C1_JP_PSE: Cluster Spacecraft 1, JSOC Predicted Scientific Events - (Non-PI) M. Hapgood (RAL)
C1_PP_ASP: Cluster Spacecraft 1, ASPOC Prime Parameters - K. Torkar (IWF-OAW)
C1_PP_CIS: Cluster Spacecraft 1, CIS Prime Parameters - I. Dandouras (IRAP)
C1_PP_DWP: Cluster Spacecraft 1, DWP Prime Parameters - M. Balikhin (Univ-Sheff)
C1_PP_EDI: Cluster Spacecraft 1, EDI Prime Parameters - R. Torbert (UNH)
C1_PP_EFW: Cluster Spacecraft 1, EFW Prime Parameters - Y. Khotyaintsev (IRFU)
C1_PP_PEA: Cluster Spacecraft 1, PEACE Prime Parameters - A. Fazakerley (MSSL)
C1_PP_RAP: Cluster Spacecraft 1, RAPID Prime Parameters - P. W. Daly (MPI Solar System Research, Goettingen, Germany)
C1_PP_STA: Cluster Spacecraft 1, STAFF Prime Parameters - N. Cornilleau-Wehrlin (LPP)
C1_PP_WHI: Cluster Spacecraft 1, WHISPER Prime Parameters - J. G. Trotignon (LPC2E)
C1_UP_FGM: Cluster Spacecraft 1, FGM Unvalidated Prime Parameters - C. Carr (ICSTM)
C1_WAVEFORM_WBD: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C1_WAVEFORM_WBD_BM2: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C2_CP_EDI_AEDC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C2_CP_EDI_MP: This dataset contains mixed (i.e. quarter- half- and one spin) resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C2_CP_EDI_QZC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C2_CP_EDI_SPIN: This dataset contains spin resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C2_CP_EFW_L3_E3D_INERT: This dataset contains 4-sec averages of the 3-dimensional Electric field vector - Yuri Khotyaintsev (IRFU)
C2_CP_EFW_L3_P: This dataset contains measurements of the - Yuri Khotyaintsev (IRFU)
C2_CP_EFW_L3_V3D_INERT: This dataset contains 4-sec averages of the ExB-drift velocity in ISR2, using - Yuri Khotyaintsev (IRFU)
C2_CP_FGM_5VPS: This dataset contains 5 vectors/second resolution measurements of the magnetic field vector from the FGM - Chris Carr (Imperial College)
C2_CP_FGM_SPIN: Cluster Spacecraft 2 FluxGate Magnetometer (FGM) Spin-Resolution Parameters
C2_CP_RAP_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C2_CP_RAP_ESPCT6: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C2_CP_RAP_HSPCT: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C2_CP_RAP_I3DM_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C2_CP_RAP_I3DM_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C2_CP_RAP_I3DM_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C2_CP_RAP_ISPCT_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C2_CP_RAP_ISPCT_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C2_CP_RAP_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C2_CP_RAP_PAD_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C2_CP_RAP_PAD_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C2_CP_RAP_PAD_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C2_CP_RAP_PAD_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C2_CP_STA_CWF_GSE: This dataset contains measurements of the magnetic field - Patrick Canu (LPP)
C2_CP_STA_PPP: Polarization and propagation parameters - Patrick Canu (LPP)
C2_CP_STA_PSD: Power Spectral Density measurements of three - Patrick Canu (LPP)
C2_CP_STA_SM: Cross spectral matrices formed from - Patrick Canu (LPP)
C2_CP_WHI_ACTIVE: This dataset contains electric spectral power density under Sounding Mode from Whisper on spacecraft 2 - Pierre Henri (LPC2E)
C2_CP_WHI_ELECTRON_DENSITY: This dataset contains plasma frequencies from Whisper on spacecraft 2 - Pierre Henri (LPC2E)
C2_CP_WHI_NATURAL: This dataset contains electric spectral power density under natural mode from Whisper on spacecraft 2 - Pierre Henri (LPC2E)
C2_CP_WHI_PASSIVE_ACTIVE: This dataset contains passive electric spectral power density under sounding mode from Whisper on spacecraft 2 - Pierre Henri (LPC2E)
C2_CP_WHI_WAVE_FORM_ENERGY: This dataset contains the Electric Wave Form Power Density under natural mode from Whisper on spacecraft 2 - Pierre Henri (LPC2E)
C2_JP_PMP: Cluster Spacecraft 2, JSOC Predicted Magnetic Positions - (Non-PI) M. Hapgood (RAL)
C2_JP_PSE: Cluster Spacecraft 2, JSOC Predicted Scientific Events - (Non-PI) M. Hapgood (RAL)
C2_PP_ASP: Cluster Spacecraft 2, ASPOC Prime Parameters - K. Torkar (IWF-OAW)
C2_PP_DWP: Cluster Spacecraft 2, DWP Prime Parameters - M. Balikhin (Univ-Sheff)
C2_PP_EDI: Cluster Spacecraft 2, EDI Prime Parameters - R. Torbert (UNH)
C2_PP_EFW: Cluster Spacecraft 2, EFW Prime Parameters - Y. Khotyaintsev (IRFU)
C2_PP_PEA: Cluster Spacecraft 2, PEACE Prime Parameters - A. Fazakerley (MSSL)
C2_PP_RAP: Cluster Spacecraft 2, RAPID Prime Parameters - P. W. Daly (MPI Solar System Research, Goettingen, Germany)
C2_PP_STA: Cluster Spacecraft 2, STAFF Prime Parameters - N. Cornilleau-Wehrlin (LPP)
C2_PP_WHI: Cluster Spacecraft 2, WHISPER Prime Parameters - J. G. Trotignon (LPC2E)
C2_UP_FGM: Cluster Spacecraft 2, FGM Unvalidated Prime Parameters - C. Carr (ICSTM)
C2_WAVEFORM_WBD: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C2_WAVEFORM_WBD_BM2: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C3_CP_CIS-CODIF_H1_1D_PEF: This dataset contains CIS-CODIF Proton omni-directional distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HE1_1D_PEF: This dataset contains CIS-CODIF Helium+ omni-directional distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_H1_PEF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_H1_PF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_H1_PSD: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_HE1_PF: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_HE1_PSD: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_O1_PEF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_O1_PF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_HS_O1_PSD: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_O1_1D_PEF: This dataset contains CIS-CODIF Oxygen+ omni-directional distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_PAD_HS_H1_PF: This dataset contains CIS-CODIF Proton Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_PAD_HS_HE1_PF: This dataset contains CIS-CODIF Helium+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C3_CP_CIS-CODIF_PAD_HS_O1_PF: This dataset contains CIS-CODIF Oxygen+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_1D_PEF: This dataset contains CIS-HIA Ion omni-directional distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_MAG_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_MAG_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_MAG_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_SW_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_SW_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_HS_SW_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_LS_1D_PEF: This dataset contains Ion omni-directional fluxes in Particle_Energy_Flux units - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_LS_SW_IONS_PEF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_LS_SW_IONS_PF: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_LS_SW_IONS_PSD: This dataset contains CIS-HIA 3D Ion distributions - Iannis Dandouras (IRAP)
C3_CP_CIS-HIA_PAD_HS_MAG_IONS_PF: This dataset contains CIS-HIA Ion Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C3_CP_EDI_AEDC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C3_CP_EDI_MP: This dataset contains mixed (i.e. quarter- half- and one spin) resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C3_CP_EDI_QZC: This dataset contains mixed resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C3_CP_EDI_SPIN: This dataset contains spin resolution measurements of the - Goetz Paschmann (University of New Hampshire)
C3_CP_EFW_L3_E3D_INERT: This dataset contains 4-sec averages of the 3-dimensional Electric field vector - Mats Andre (IRFU)
C3_CP_EFW_L3_P: This dataset contains measurements of the - Yuri Khotyaintsev (IRFU)
C3_CP_EFW_L3_V3D_INERT: This dataset contains 4-sec averages of the ExB-drift velocity in ISR2, using - Mats Andre (IRFU)
C3_CP_FGM_5VPS: This dataset contains 5 vectors/second resolution measurements of the magnetic field vector from the FGM - Chris Carr (Imperial College)
C3_CP_FGM_SPIN: Cluster Spacecraft 3 FluxGate Magnetometer (FGM) Spin-Resolution Parameters
C3_CP_RAP_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C3_CP_RAP_ESPCT6: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C3_CP_RAP_HSPCT: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C3_CP_RAP_I3DM_CNO: This dataset contains differential fluxes of CNO - Berend Wilken (MPS)
C3_CP_RAP_I3DM_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C3_CP_RAP_I3DM_HE: This dataset contains differential fluxes of Helium - Berend Wilken (MPS)
C3_CP_RAP_ISPCT_CNO: This dataset contains differential fluxes of CNO - Berend Wilken (MPS)
C3_CP_RAP_ISPCT_HE: This dataset contains differential fluxes of Helium - Berend Wilken (MPS)
C3_CP_RAP_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C3_CP_RAP_PAD_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C3_CP_RAP_PAD_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C3_CP_RAP_PAD_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C3_CP_RAP_PAD_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C3_CP_RAP_PAD_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C3_CP_STA_CWF_GSE: This dataset contains measurements of the magnetic field - Patrick Canu (LPP)
C3_CP_STA_PPP: Polarization and propagation parameters - Patrick Canu (LPP)
C3_CP_STA_PSD: Power Spectral Density measurements of three - Patrick Canu (LPP)
C3_CP_STA_SM: Cross spectral matrices formed from - Patrick Canu (LPP)
C3_CP_WHI_ACTIVE: This dataset contains electric spectral power density under Sounding Mode from Whisper on spacecraft 3 - Pierre Henri (LPC2E)
C3_CP_WHI_ELECTRON_DENSITY: This dataset contains plasma frequencies from Whisper on spacecraft 3 - Pierre Henri (LPC2E)
C3_CP_WHI_NATURAL: This dataset contains electric spectral power density under natural mode from Whisper on spacecraft 3 - Pierre Henri (LPC2E)
C3_CP_WHI_PASSIVE_ACTIVE: This dataset contains passive electric spectral power density under sounding mode from Whisper on spacecraft 3 - Pierre Henri (LPC2E)
C3_CP_WHI_WAVE_FORM_ENERGY: This dataset contains the Electric Wave Form Power Density under natural mode from Whisper on spacecraft 3 - Pierre Henri (LPC2E)
C3_JP_PMP: Cluster Spacecraft 3, JSOC Predicted Magnetic Positions - (Non-PI) M. Hapgood (RAL)
C3_JP_PSE: Cluster Spacecraft 3, JSOC Predicted Scientific Events - (Non-PI) M. Hapgood (RAL)
C3_PP_ASP: Cluster Spacecraft 3, ASPOC Prime Parameters - K. Torkar (IWF-OAW)
C3_PP_CIS: Cluster Spacecraft 3, CIS Prime Parameters - I. Dandouras (IRAP)
C3_PP_EDI: Cluster Spacecraft 3, EDI Prime Parameters - R. Torbert (UNH)
C3_PP_EFW: Cluster Spacecraft 3, EFW Prime Parameters - Y. Khotyaintsev (IRFU)
C3_PP_PEA: Cluster Spacecraft 3, PEACE Prime Parameters - A. Fazakerley (MSSL)
C3_PP_RAP: Cluster Spacecraft 3, RAPID Prime Parameters - P. W. Daly (MPI Solar System Research, Goettingen, Germany)
C3_PP_STA: Cluster Spacecraft 3, STAFF Prime Parameters - N. Cornilleau-Wehrlin (LPP)
C3_PP_WHI: Cluster Spacecraft 3, WHISPER Prime Parameters - J. G. Trotignon (LPC2E)
C3_UP_FGM: Cluster Spacecraft 3, FGM Unvalidated Prime Parameters - C. Carr (ICSTM)
C3_WAVEFORM_WBD: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C3_WAVEFORM_WBD_BM2: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C4_CP_CIS-CODIF_H1_1D_PEF: This dataset contains CIS-CODIF Proton omni-directional distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HE1_1D_PEF: This dataset contains CIS-CODIF Helium+ omni-directional distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HE1_DENSITY_CORRECTED: He+ density (with standard devitation), which is - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_H1_PEF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_H1_PF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_H1_PSD: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_HE1_PF: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_HE1_PSD: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_O1_PEF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_O1_PF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_HS_O1_PSD: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_H1_PEF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_H1_PF: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_H1_PSD: This dataset contains CIS-CODIF 3D Proton distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_HE1_PEF: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_HE1_PF: This dataset contains CIS-CODIF 3D Helium+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_O1_PEF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_O1_PF: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_LS_O1_PSD: This dataset contains CIS-CODIF 3D Oxygen+ distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_O1_1D_PEF: This dataset contains CIS-CODIF Oxygen+ omni-directional distributions - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_HS_H1_PF: This dataset contains CIS-CODIF Proton Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_HS_HE1_PF: This dataset contains CIS-CODIF Helium+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_HS_O1_PF: This dataset contains CIS-CODIF Oxygen+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_LS_H1_PF: This dataset contains CIS-CODIF Proton Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_LS_HE1_PF: This dataset contains CIS-CODIF Helium+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_CIS-CODIF_PAD_LS_O1_PF: This dataset contains CIS-CODIF Oxygen+ Pitch-Angle Distribution, - Iannis Dandouras (IRAP)
C4_CP_EFW_L3_E3D_INERT: This dataset contains 4-sec averages of the 3-dimensional Electric field vector - Yuri Khotyaintsev (IRFU)
C4_CP_EFW_L3_P: This dataset contains measurements of the - Yuri Khotyaintsev (IRFU)
C4_CP_EFW_L3_V3D_INERT: This dataset contains 4-sec averages of the ExB-drift velocity in ISR2, using - Yuri Khotyaintsev (IRFU)
C4_CP_FGM_5VPS: This dataset contains 5 vectors/second resolution measurements of the magnetic field vector from the FGM - Chris Carr (Imperial College)
C4_CP_FGM_SPIN: Cluster Spacecraft 4 FluxGate Magnetometer (FGM) Spin-Resolution Parameters
C4_CP_RAP_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C4_CP_RAP_ESPCT6: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C4_CP_RAP_HSPCT: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C4_CP_RAP_I3DM_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C4_CP_RAP_I3DM_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C4_CP_RAP_I3DM_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C4_CP_RAP_ISPCT_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C4_CP_RAP_ISPCT_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C4_CP_RAP_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C4_CP_RAP_PAD_CNO: This dataset contains differential fluxes of CNO ions - Berend Wilken (MPS)
C4_CP_RAP_PAD_E3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C4_CP_RAP_PAD_H: This dataset contains differential fluxes of Protons - Berend Wilken (MPS)
C4_CP_RAP_PAD_HE: This dataset contains differential fluxes of Helium ions - Berend Wilken (MPS)
C4_CP_RAP_PAD_L3DD: This dataset contains differential fluxes of Electrons - Berend Wilken (MPS)
C4_CP_STA_CWF_GSE: This dataset contains measurements of the magnetic field - Patrick Canu (LPP)
C4_CP_STA_PPP: Polarization and propagation parameters - Patrick Canu (LPP)
C4_CP_STA_PSD: Power Spectral Density measurements of three - Patrick Canu (LPP)
C4_CP_STA_SM: Cross spectral matrices formed from - Patrick Canu (LPP)
C4_CP_WHI_ACTIVE: This dataset contains electric spectral power density under Sounding Mode from Whisper on spacecraft 4 - Pierre Henri (LPC2E)
C4_CP_WHI_ELECTRON_DENSITY: This dataset contains plasma frequencies from Whisper on spacecraft 4 - Pierre Henri (LPC2E)
C4_CP_WHI_NATURAL: This dataset contains electric spectral power density under natural mode from Whisper on spacecraft 4 - Pierre Henri (LPC2E)
C4_CP_WHI_PASSIVE_ACTIVE: This dataset contains passive electric spectral power density under sounding mode from Whisper on spacecraft 4 - Pierre Henri (LPC2E)
C4_CP_WHI_WAVE_FORM_ENERGY: This dataset contains the Electric Wave Form Power Density under natural mode from Whisper on spacecraft 4 - Pierre Henri (LPC2E)
C4_JP_PMP: Cluster Spacecraft 4, JSOC Predicted Magnetic Positions - (Non-PI) M. Hapgood (RAL)
C4_JP_PSE: Cluster Spacecraft 4, JSOC Predicted Scientific Events - (Non-PI) M. Hapgood (RAL)
C4_PP_ASP: Cluster Spacecraft 4, ASPOC Prime Parameters - K. Torkar (IWF-OAW)
C4_PP_CIS: Cluster Spacecraft 4, CIS Prime Parameters - I. Dandouras (IRAP)
C4_PP_DWP: Cluster Spacecraft 4, DWP Prime Parameters - M. Balikhin (Univ-Sheff)
C4_PP_EDI: Cluster Spacecraft 4, EDI Prime Parameters - R. Torbert (UNH)
C4_PP_EFW: Cluster Spacecraft 4, EFW Prime Parameters - Y. Khotyaintsev (IRFU)
C4_PP_PEA: Cluster Spacecraft 4, PEACE Prime Parameters - A. Fazakerley (MSSL)
C4_PP_RAP: Cluster Spacecraft 4, RAPID Prime Parameters - P. W. Daly (MPI Solar System Research, Goettingen, Germany)
C4_PP_STA: Cluster Spacecraft 4, STAFF Prime Parameters - N. Cornilleau-Wehrlin (LPP)
C4_PP_WHI: Cluster Spacecraft 4, WHISPER Prime Parameters - J. G. Trotignon (LPC2E)
C4_UP_FGM: Cluster Spacecraft 4, FGM Unvalidated Prime Parameters - C. Carr (ICSTM)
C4_WAVEFORM_WBD: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
C4_WAVEFORM_WBD_BM2: Cluster Wideband Data Plasma Wave Receiver/High Time Resolution Waveform Data - 2006 - Current: J. S. Pickett; 1988 - 2006: D. A. Gurnett (The University of Iowa)
CASSINI_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
CASSINI_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
CASSINI_MAG_1MIN_MAGNETIC_FIELD: 1 min averaged magnetic field - Michele Dougherty (Imperial College, London)
CIRBE_REPTILE-2_L1A_DETECTORS: Colorado Inner Radiation Belt Experiment, Relativistic Electron Proton Telescope integrated little experiment-2, Level 1A Data Product, Detectors - Xinlin Li (University of Colorado at Boulder)
CIRBE_REPTILE-2_L1B_RNG_ELECS: Colorado Inner Radiation Belt Experiment, Relativistic Electron Proton Telescope integrated little experiment-2, Level 1B Data Product, Range Electrons - Xinlin Li (University of Colorado at Boulder)
CIRBE_REPTILE-2_L2_RNG_ELECS: Colorado Inner Radiation Belt Experiment, Relativistic Electron-Proton Telescope integrated little experiment-2, Level 2 Data Product, Range Electrons - Xinlin Li (University of Colorado at Boulder)
CL_JP_PCY: Cluster, JSOC Predicted Solar Cycle Trends - (Non-PI) M. Hapgood (RAL)
CL_JP_PGP: Cluster, JSOC Predicted Geometric Positions - (Non-PI) M. Hapgood (RAL)
CL_OR_GIFWALK: Link to Cluster orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
CL_SP_AUX: Cluster, Auxiliary Parameters - (Non-PI) M. Tatrallyay (Wigner RCP, RMKI)
CNOFS_CINDI_IVM_500MS: CNOFS CINDI IVM ion density, composition, temperature, and drift (0.5-sec) - Dr. Roderick A. Heelis (University of Texas, Dallas)
CNOFS_PLP_PLASMA_1SEC: C/NOFS Planar Langmuir Probe 1 second average Key Parameters. "The data are PRELIMINARY, and as such, are intended for BROWSE PURPOSES ONLY" - D. E. Hunton (Air Force Research Laboratory, Space Vehicles Directorate)
CNOFS_VEFI_BFIELD_1SEC: Magnetic field solution (at 1 sample per sec) produced by VEFI on the Communication Navigation Outage Forecast System satellite. - Robert F. Pfaff (NASA GSFC)
CNOFS_VEFI_EFIELD_1SEC: Electric Field solution (at 1 sample/sec) produced by VEFI on the Communication Navigation Outage Forecast System satellite. The data are PRELIMINARY, and as such, are intended for BROWSE PURPOSES ONLY. - Robert F. Pfaff (GSFC)
CNOFS_VEFI_LD_500MS: CNOFS VEFI Lightning Detector, low rate data (eclipse portion of CNOFS orbit) - Robert H. Holzworth (University of Washington)
CN_K0_ASI: CANOPUS All Sky Imager, Key Parameters - J. Samson (U. Alberta)
CN_K0_BARS: CANOPUS Bistatic Auroral Radar System, Key Parameters - John Samson (University of Alberta)
CN_K0_MARI: CANOPUS MARI Magnetometer Key Parameters - J. Samson (U. Alberta)
CN_K0_MPA: CANOPUS Meridian Photometer Array, Key Parameters - J. Samson (U. Alberta)
CN_K1_MARI: CANOPUS MARI Riometer Key Parameters - J. Samson (U. Alberta)
COMETGS_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
COMETGS_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
COMETHMP_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
COMETHMP_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
CRRES_H0_MEA: CRRES-MEA Data Archive - TBD (NSSDC)
CSSWE_REPTILE_6SEC-COUNTS-L1: CSSWE REPTile level1 6sec Counts and Position - Xinlin Li (University of Colorado at Boulder)
CSSWE_REPTILE_6SEC-FLUX-L2: CSSWE REPTile level2 6sec flux and Position - Xinlin Li (University of Colorado at Boulder)
CT_JP_PSE: Cluster centroid, JSOC Predicted Scientific Events - (Non-PI) M. Hapgood (RAL)
DAWN_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
DAWN_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
DE1_1MIN_RIMS: DE-1 Retarding Ion Mass Spectrometer Empirical Model - Dr. Charles R. Chappell (NASA/MSFC)
DE1_2SEC_OA: de1 2 second orbit and additude data - David Winningham (Southwest Research Institute)
DE1_62MS_MAGA-GMS: DE-1 Magnetometer (MAG-A) 62.5 msec GMS Data - Dr. Masahisa Sugiura (NASA/GSFC)
DE1_6SEC_MAGAGMS: DE-1 Magnetometer (MAG-A) 6 second GMS Data - Dr. Masahisa Sugiura (NASA/GSFC)
DE1_PWI_LFC-SPECTRA: DE-1 PWI: LOW Frequency Correlator (LFC) - Donald Gurnett (University Iowa)
DE1_PWI_OR-AT: DE-1 PWI: Ephemeris and Attitude Parameters - Donald Gurnett (University Iowa)
DE1_PWI_SFC-SPECTRA: DE-1 PWI: Step Frequency Correlator (SFC) - Donald Gurnett (University Iowa)
DE2_62MS_VEFIMAGB: 16-msec merged magnetic and electric field data - Jim Slavin (NASA/GSFC)
DE2_AC500MS_VEFI: 500-msec AC data from each channel for each of the 3 spectrometers of the vector electric field instrument - N.C. Maynard/R. Pfaff (NASA/GSFC)
DE2_DCA500MS_VEFI: 500-msec spectrometer vector electric field instrument - Dr. Nelson C. Maynard (NASA/GSFC)
DE2_DUCT16MS_RPA: De-2 duct 16ms rpa - William Hanson (University of Texas, Dallas)
DE2_ION2S_RPA: 2-sec ion temperature, velocity, and densities (O+, H+, He+, molecular) - Rod Heelis (University of Texas, Dallas)
DE2_LAPI_ELECTRON-FLUX-COUNTS-PPS1: DE-2, LAPI_Corrected Electron Counts and Flux from Power Supply 1 IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_ELECTRON-FLUX-COUNTS-PPS2: DE-2, LAPI_Corrected Electron Counts and Flux from Power Supply 2 IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_GEIGER-MUELLER: DE-2, LAPI_Corrected IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_GEIGER-MUELLER-RATIO: DE-2, LAPI_Corrected IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_ION-FLUX-COUNTS-PPS1: DE-2, LAPI_Corrected Ion Counts and Flux from Power Supply 1 IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_ION-FLUX-COUNTS-PPS2: DE-2, LAPI_Corrected Ion Counts and Flux from Power Supply 2 IDFS format - Dr. J. David Winningham (Southwest Research Institute)
DE2_LAPI_LAPI-MAG: DE-2, LAPI_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_ORBIT-ATTITUDE: DE-2, OA_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_ORBIT-ATTITUDE-MAGB: DE-2, OA_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_PITCH-ANGLES: DE-2, LAPI_Corrected Precopitation and Pitch Angles IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_PROJECTED-MAGB: DE-2, MAGB_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_SC-MAGB: DE-2, MAGB_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_LAPI_SHAFT-ENCODER-ANGLE: DE-2, LAPI_Corrected IDFS format - David Winningham (Southwest Research Institute)
DE2_NEUTRAL1S_NACS: 1-sec ambient densities and error rates - Nelson W. Spencer (NASA/GSFC)
DE2_NEUTRAL8S_FPI: 8-sec neutral wind and temperature data from FPI plus WATS - Dr. R. Niciejewski (University of Michigan)
DE2_PLASMA500MS_LANG: .5 sec electron temperature, plasma density, and satellite potential - Larry H. Brace (NASA/GSFC)
DE2_UA16S_ALL: 16-sec combined neutral and plasma unified abstract (UA) data - Mr. Larry H. Brace (NASA/GSFC)
DE2_VION250MS_IDM: 250-msec cross track ion drift velocities - Rod Heelis (University of Texas, Dallas)
DE2_WIND2S_WATS: 2-sec neutral densities, temperature, and horizontal (zonal) wind velocity - Nelson W. Spencer (NASA/GSFC)
DE_UV_SAI: DE-1 Spin-scan Auroral Imager (SAI) Ultraviolet Images - Louis A. Frank (The University of Iowa)
DE_VS_EICS: Dynamics Explorer Energetic Ion Composition Spectrometer (EICS), Validated Summary Data - E. G. Shelley (Lockheed Martin)
DMSP-F06_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F07_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F08_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F09_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F12_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F13_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F14_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F15_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F16_SSIES-3_THERMAL-PLASMA: DMSP thermal plasma data - William Hanson, Rod Heelis, Marc Hairston (University of Texas Dallas, Center for Space Sciences)
DMSP-F16_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F16_SSM_MAGNETOMETER: Defense Meteorolgy Satellite Program F16 Vector Magnetometer Measurements (850km Altitude) - Staff (AFRL, NGDC, CU)
DMSP-F17_SSIES-3_THERMAL-PLASMA: DMSP thermal plasma data - William Hanson, Rod Heelis, Marc Hairston (University of Texas Dallas, Center for Space Sciences)
DMSP-F17_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F17_SSM_MAGNETOMETER: Defense Meteorolgy Satellite Program F17 Vector Magnetometer Measurements (850km Altitude) - Staff (AFRL, NGDC, CU)
DMSP-F18_SSIES-3_THERMAL-PLASMA: DMSP thermal plasma data - William Hanson, Rod Heelis, Marc Hairston (University of Texas Dallas, Center for Space Sciences)
DMSP-F18_SSJ_PRECIPITATING-ELECTRONS-IONS: Precipitating electrons and ions observed at nominally 850km. - Staff (AFRL, NGDC, CU)
DMSP-F18_SSM_MAGNETOMETER: Defense Meteorolgy Satellite Program F18 Vector Magnetometer Measurements (850km Altitude) - Staff (AFRL, NGDC, CU)
DMSPF16_R0_SSUSI: Links to DMSP F16 SSUSI NetCDF data, KZM image files and other sources. - Larry Paxton (JHUAPL)
DMSPF17_R0_SSUSI: Links to DMSP F17 SSUSI NetCDF data, KZM image files and other sources. - Larry Paxton (JHUAPL)
DMSPF18_R0_SSUSI: Links to DMSP F18 SSUSI NetCDF data, KMZ image files and other sources. - Larry Paxton (JHUAPL)
DMSP_R0_SSIES: Link to DMSP thermal plasma analysis package data service at the Center for Space Sciences, University of Texas at Dallas. - Center for Space Sciences (UTD)
DMSP_R0_SSJ4: Link to DMSP low energy electron/ion plots and data at JHU/APL - Hardy (AFGL)
DN_K0_GBAY: DARN Goose Bay, Key Parameters - R. Greenwald (JHU/APL)
DN_K0_HANK: DARN Hankasalmi, Key Parameters - R. Greenwald (JHU/APL)
DN_K0_ICEW: DARN Iceland West (Stokkseyri),Key Parameters - R. Greenwald (JHU/APL)
DN_K0_KAPU: DARN Kapuskasing,Key Parameters - R. Greenwald (JHU/APL)
DN_K0_PACE: DARN PACE, Key Parameters - R. Greenwald (JHU/APL)
DN_K0_PYKK: DARN Pykkvibaer, Key Parameters - R. Greenwald (JHU/APL)
DN_K0_SASK: DARN Saskatoon, Key Parameters - R. Greenwald (JHU/APL)
DN_MAGN-L2-HIRES_G08: GOES-08 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G09: GOES-09 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G10: GOES-10 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G11: GOES-11 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G12: GOES-12 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G13: GOES-13 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G14: GOES-14 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G15: GOES-15 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G16: GOES-16 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G17: GOES-17 Magnetometer L2 - Rob Redmon, Paul Loto'aniu, Howard Singer (DOC/NOAA/NCEI and DOC/NOAA/NWS/SWPC respectively)
DN_MAGN-L2-HIRES_G18: GOES-18 Magnetometer L2 - Rob Redmon, Paul Loto'aniu (DOC/NOAA/NESDIS/NCEI/OGSSD/STP)
DN_MAGN-L2-HIRES_G19: GOES-19 Magnetometer L2 Geomagnetic Field 10 Hz Product with Complete Coordinate Frames - Rob Redmon, Paul Loto'aniu (DOC/NOAA/NESDIS/NCEI/OGSSD/STP)
DSCOVR_AT_DEF: DSCOVR Definitive Attitude - A. Szabo (NASA Goddard Space Flight Center)
DSCOVR_AT_PRE: DSCOVR Preliminary Attitude - A. Szabo (NASA Goddard Space Flight Center)
DSCOVR_H0_MAG: DSCOVR Fluxgate Magnetometer 1-sec Definitive Data - A. Koval (UMBC, NASA/GSFC)
DSCOVR_H1_FC: Isotropic Maxwellian parameters for solar wind protons. - Justin C. Kasper (Smithonian Astrophysical Observatory)
DSCOVR_ORBIT_PRE: DSCOVR Predicted Orbit - A. Szabo (NASA Goddard Space Flight Center)
DYNAMO-2_DESA_NX02A-ESA-FLUX: Standard Resolution (15% DE/E) data (0.5eV to 1keV) - G. Collinson (NASA GSFC / Catholic University of America)
EARTH_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
EARTH_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
ELA_L1_EPDEF: Energetic Particle Detector, Counts, Electrons>keV [UNCALIBRATED RAW DATA] - V. Angelopoulos (UCLA, IGPP/EPSS)
ELA_L1_EPDIF: [UNCALIBRATED RAW DATA ONLY] Energetic Partical Detector Energy Particles, Ions>keV - V. Angelopoulos (UCLA, IGPP/EPSS)
ELA_L1_STATE_DEFN: Probe state file, contains position and attitude and orbit events - V. Angelopoulos (UCLA, IGPP/EPSS)
ELA_L1_STATE_PRED: Probe state file, contains position and attitude and orbit events - V. Angelopoulos (UCLA, IGPP/EPSS)
ELB_L1_EPDEF: Energetic Particle Detector, Counts, Electrons>keV [UNCALIBRATED RAW DATA] - V. Angelopoulos (UCLA, IGPP/EPSS)
ELB_L1_EPDIF: [UNCALIBRATED RAW DATA ONLY] Energetic Partical Detector Energy Particles, Ions>keV - V. Angelopoulos (UCLA, IGPP/EPSS)
ELB_L1_STATE_DEFN: Probe state file, contains position and attitude and orbit events - V. Angelopoulos (UCLA, IGPP/EPSS)
ELB_L1_STATE_PRED: Probe state file, contains position and attitude and orbit events - V. Angelopoulos (UCLA, IGPP/EPSS)
ENDURANCE_EPHEMERIS_DEF: Position and attitude of Endurance during flight - G. Collinson (NASA GSFC / Catholic University of America)
ENDURANCE_EPHEMERIS_GPS: Endurance GPS Velocity, Position, Altitude, and Magnetic Latitude and Longitude - G. Collinson (NASA GSFC / Catholic University of America)
ENDURANCE_FIELDS_SKINPOT-500US: Electric field sphere voltages. - G. Collinson (NASA GSFC / Catholic University)
ENDURANCE_FIELDS_VLF-33US: Electric field differential sphere voltages. - G. Collinson (NASA GSFC / Catholic University)
ENDURANCE_L1A_PES: Level 1a PES Science and Housekeeping data at 40ms time resolution as downlinked in the Data Matrix - G. Collinson (NASA GSFC / Catholic University of America )
ENDURANCE_L1B_PES: Uncalibrated L1b raw counts per energy step from the 8 DESA sensors during science portion of mission - G. Collinson (NASA GSFC / Catholic University of America )
ENDURANCE_L2-ESA_PES: Standard Resolution (15% DE/E) data (10eV to 1keV) - G. Collinson (NASA GSFC / Catholic University of America )
ENDURANCE_L2-GF_PES: Variation of Geometric Factor of PES during operation - G. Collinson (NASA GSFC / Catholic University of America )
ENDURANCE_L2-RPA_PES: High Resolution (0.5% DE/E) data (20.30eV to 25.85eV) - G. Collinson (NASA GSFC / Catholic University of America )
ENDURANCE_L2_SLP: Calibrated L2 data from SLP - A. Barjatya (Embry Riddle Aeronautical University)
ENDURANCE_L2_SLP_PSD: Sweeping Langmuir Probe (SLP) power spectral density. - G. Collinson (NASA GSFC / Catholic University)
ENDURANCE_L3_PES: Electric Potential Drop parallel to Earth’s magnetic Field below Endurance - G. Collinson (NASA GSFC / Catholic University of America )
EQ_PP_AUX: Equator-S Auxiliary Data Prime Parameters - EDC (MPE)
EQ_PP_EDI: Equator-S Electron Drift Instrument Prime Parameters - G. Paschmann (MPE)
EQ_PP_EPI: Equator-S 3D Analyzer Prime Parameters - T. Sanderson (ESTEC)
EQ_PP_ICI: Equator-S Ion Composition Instrument Prime Parameters.(The raw moments calculated onboard should only be used qualitatively for identifying regions and temporal variations. Quantitative analysis should be done with the final moments generated from telemetered 3D distributions.) - L. Kistler (UNH)
EQ_PP_MAM: Equator-S Fluxgate Magnetometer Prime Parameters - W. Baumjohann (MPE)
EQ_PP_PCD: Equator-S Potential Control Device Prime Parameters - K. Torkar (IWF)
EQ_SP_SFD: Equator-S Scintillating Fibre Detector Summary Parameters - L. Adams (ESTEC)
ERG_HEP_L2_OMNIFLUX: High-energy electron experiments (HEP) Level-2 omni flux data, ARASE/ERG) - Takefumi Mitani (ISAS, JAXA)
ERG_LEPE_L2_OMNIFLUX: Low-Energy Particle experiments - electron analyzer (LEP-e) Level 2 omni electron flux data, ARASE/ERG - Shiang-Yu Wang (Academia Sinica, Taiwan)
ERG_LEPI_L2_OMNIFLUX: Exploration of Low Energy Particle Ion (LEPi) Experiment 3D ion flux data, ARASE/ERG - Kazushi Asamura (ISAS, Jaxa)
ERG_MEPE_L2_3DFLUX: Exploration of Energization and Radiation in Geospace (ERG) Medium-Energy Particle experiments - electron analyzer (MEP-e) Level 2 3D electron flux data - Satoshi Kasahara (The University of Tokyo)
ERG_MEPE_L2_OMNIFLUX: Medium Energy Particle experiments - electron analyzer (MEP-e) electron omni flux data, ARASE/ERG - Satoshi Kasahara (The University of Tokyo)
ERG_MEPI_L2_3DFLUX: Exploration of Energization and Radiation in Geospace (ERG) Medium Energy Particle experiments - ion mass analyzer (MEP-i) Level-2 3D flux data - Shoichiro Yokota (Osaka University)
ERG_MEPI_L2_OMNIFLUX: Medium Energy Particle experiments - ion mass analyzer (MEP-i) 3D ion omni flux data, ARASE/ERG - Shoichiro Yokota (Osaka University)
ERG_MGF_L2_8SEC: Magnetic Field Experiment (MGF) Level 2 spin-averaged magnetic field data, ARASE/ERG - Ayako Matsuoka (Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa 252-5210, Japan)
ERG_ORB_L2: Exploration of Energization and Radiation in Geospace (ERG) Level-2 orbit data
ERG_ORB_LPRE_L2: Exploration of Energization and Radiation in Geospace (ERG) Level-2 long-term predicted orbit data
ERG_ORB_MPRE_L2: Exploration of Energization and Radiation in Geospace (ERG) Level-2 medium-term predicted orbit data
ERG_ORB_PRE_L2: Exploration of Energization and Radiation in Geospace (ERG) Level-2 predicted orbit data
ERG_ORB_SPRE_L2: Exploration of Energization and Radiation in Geospace (ERG) Level-2 short-term predicted orbit data
ERG_PWE_EFD_L2_E_SPIN: Plasma Wave Experiment (PWE) Electric Field Detector (EFD) Level 2 spectrum data, ARASE/ERG - Yoshiya Kasahara (Kanazawa University)
ERG_PWE_EFD_L2_POT: Plasma Wave Experiment (PWE) Electric Field Detector (EFD) Level 2 potential data, ARASE/ERG - Yoshiya Kasahara (Kanazawa University)
ERG_PWE_HFA_L2_SPEC_HIGH: No description
ERG_PWE_HFA_L2_SPEC_LOW: No description
ERG_PWE_HFA_L2_SPEC_MONIT: No description
ERG_PWE_OFA_L2_SPEC: Plasma Wave Experiment (PWE) Onboard Frequency Analyzer (OFA) Level 2 spectrum data, ARASE/ERG - Yoshiya Kasahara (Kanazawa University)
ERG_XEP_L2_OMNIFLUX: Exploration of Energization and Radiation in Geospace (ERG) Extremely High-Energy Electron Experiment (XEP) Level 2 extremely high energy electron data - Nana Higashio (Space Environment Group, Aerospace Research and Development Directorate, Tsukuba Space Center, Japan Aerospace Exploration Agency, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan)
FAST_HR_DCB: High-resolution Fluxgate Magnetometer data for the FAST Mission - Robert Strangeway (UCLA)
FAST_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
FAST_TEAMS_PA_L2: FAST TEAMS Energy-Pitch Angle Distributions - Lynn Kistler (University of New Hampshire)
FA_ESA_L2_EEB: FAST Ion and Electron Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
FA_ESA_L2_EES: FAST Ion and Electron Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
FA_ESA_L2_IEB: FAST Ion and Electron Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
FA_ESA_L2_IES: FAST Ion and Electron Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
FA_K0_ACF: FAST AC Fields - Key Parameters - C. Carlson (U.C. Berkeley)
FA_K0_TMS: FAST TEAMS - Key Parameters - C. Carlson (U.C. Berkeley)
FM_K0_KILP: FMI Kilpisjarvi: All-Sky Camera Key Parameters - K. Kauristie (Finnish Meteorological Institute)
FORMOSAT5_AIP_IDN: FORMOSAT-5, Advanced Ionospheric Probe, Ion Density - C.K. Chao (NCU)
G0_K0_EP8: GOES 10 Energetic Particle Sensor, Key Parameters - T. Onsager (NOAA SEC)
G0_K0_GIFWALK: Links to GEOSYNC KP pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
G0_K0_MAG: GOES 10 Magnetometer Key Parameters - H. Singer (NOAA SEC)
G10_L2_MAG: GOES-10 ephemeris and magnetometer data - Howard J. Singer (NOAA Space Weather Prediction Center)
G11_L2_MAG: GOES-11 ephemeris and magnetometer data - Howard J. Singer (NOAA Space Weather Prediction Center)
G12_L2_MAG: GOES-12 ephemeris and magnetometer data - Howard J. Singer (NOAA Space Weather Prediction Center)
G6_K0_EPS: GOES 6 Energetic Particle Sensor, Key Parameters - H. Sauer (NOAA)
G6_K0_MAG: GOES-6 Magnetometer Key Parameters - R. Zwickl (NOAA SEL)
G7_K0_EPS: GOES 7 Energetic Particle Sensor, Key Parameters - H. Sauer (NOAA)
G7_K0_MAG: GOES-7 Magnetometer Key Parameters - R. Zwickl (NOAA SEL)
G7_K1_MAG: GOES-7 Magnetometer Calculated PSD for Hn - R. Zwickl (NOAA SEL)
G8_K0_EP8: GOES 8 Energetic Particle Sensor, Key Parameters - T. Onsager (NOAA SEC)
G8_K0_MAG: GOES 8 Magnetometer Key Parameters - H. Singer (NOAA SEC)
G9_K0_EP8: GOES 9 Energetic Particle Sensor, Key Parameters - T. Onsager (NOAA SEC)
G9_K0_MAG: GOES 9 Magnetometer Key Parameters - H. Singer (NOAA SEC)
GALILEO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GALILEO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GENESIS_3DL2_GIM: Genesis Ion Monitor Experiment - Roger C. Wiens (LANL)
GE_1MIN_MAG_PLASMA_SW_ONLY: Geotail Combined, Definitive, Minute IMF, Plasma - J.H. King, N. Papatashvilli (Perot Sys, NASA GSFC)
GE_AT_DEF: Geotail Definitive Attitude
GE_AT_PRE: Geotail Predicted Attitude
GE_EDA12SEC_LEP: Editor-A 12 second, Low-Energy Particles, Geotail - T. Mukai (ISAS)
GE_EDA3SEC_MGF: Editor-A 3 second data, Magnetic Field Instrument, Geotail - S. Kokubun (STELAB Nagoya Univ., Japan)
GE_EDB12SEC_LEP: Editor-B 12 second, Low-Energy Particles, Geotail - T. Mukai (ISAS)
GE_EDB3SEC_MGF: Editor-B 3 second data, Magnetic Field Instrument, Geotail - S. Kokubun (STELAB Nagoya Univ., Japan)
GE_H0_CPI: Plasma Moments, Definitive Geotail CPI/SWA (Comprehensive Plasma Instrument / Solar Wind Analyzer) - L. Frank, W. Patterson and K. Ackerson (U. Iowa)
GE_HPAMOM_CPI: Geotail Comprehensive Plasma Inst., 45s HPA Bulk Parameters - L. Frank (U. Iowa)
GE_K0_CPI: Geotail Comprehensive Plasma Inst (CPI), Key Parameters - L. Frank (U. Iowa)
GE_K0_EFD: Geotail Electric Field Detector, Key Parameters - K. Tsuruda (ISAS)
GE_K0_EPI: Geotail Energetic Particles & Ion Composition (EPIC), Key Parameters - D. Williams (APL/JHU)
GE_K0_GIFWALK: Links to Geotial pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
GE_K0_LEP: Geotail Low-Energy Particles, Key Parameters - T. Mukai (ISAS)
GE_K0_MGF: Geotail Magnetic Field Instrument - S. Kokubun (STELAB Nagoya Univ., Japan)
GE_K0_PWI: Geotail Plasma Wave Instrument, Key Parameters - H. Matsumoto (Kyoto Univ.)
GE_K0_SPHA: Geotail Spin Phase
GE_OR_DEF: Geotail Definitive Orbit
GE_OR_GIFWALK: Links to Geotail and multi-mission orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
GE_OR_PRE: Geotail Predicted Orbit
GE_SW_CPI: Distributions and Plasma Moments, Definitive, Geotail CPI/SWA (Comprehensive Plasma Instrument / Solar Wind Analyzer) - L. Frank, W. Patterson and K. Ackerson (U. Iowa)
GIACOBINI_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GIACOBINI_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GIOTTO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GIOTTO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
GOES10_EPHEMERIS_SSC: GOES10 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES11_EPHEMERIS_SSC: GOES11 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES11_K0_EP8: GOES 11 Energetic Particle Sensor, Key Parameters - T. Onsager (NOAA SEC)
GOES11_K0_MAG: GOES 11 Magnetometer Key Parameters - H. Singer (NOAA SEC)
GOES12_EPHEMERIS_SSC: GOES12 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES12_K0_MAG: GOES 12 Magnetometer Key Parameters - H. Singer (NOAA SEC)
GOES13_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN: GOES Energetic Proton Electron and Alpha Detector Electron Fluxes reprocessed for scientific use - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES13_EPHEMERIS_SSC: GOES13 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES13_EPS-MAGED_1MIN: GOES-13 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES13_EPS-MAGED_5MIN: GOES-13 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 5 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES13_EPS-PITCH-ANGLES_1MIN: GOES-13 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES14_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN: GOES Energetic Proton Electron and Alpha Detector Electron Fluxes reprocessed for scientific use - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES14_EPHEMERIS_SSC: GOES14 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES14_EPS-MAGED_1MIN: GOES-14 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES14_EPS-MAGED_5MIN: GOES-14 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 5 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES14_EPS-PITCH-ANGLES_1MIN: GOES-14 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES15_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN: GOES Energetic Proton Electron and Alpha Detector Electron Fluxes reprocessed for scientific use - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES15_EPHEMERIS_SSC: GOES-15 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES15_EPS-MAGED_1MIN: GOES-15 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES15_EPS-MAGED_5MIN: GOES-15 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 5 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES15_EPS-PITCH-ANGLES_1MIN: GOES-15 EPS (Energetic Particle Sensor) MagED (Magnetospheric Electron Detector) 1 minute electron fluxes 40-475 keV - NOAA NGDC and SWPC (sem.goes@noaa.gov)
GOES16_EPHEMERIS_SSC: GOES16 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES17_EPHEMERIS_SSC: GOES17 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES18_EPHEMERIS_SSC: GOES-18 ephemeris data generated by the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES8_EPHEMERIS_SSC: GOES8 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOES9_EPHEMERIS_SSC: GOES9 Ephemeris data from the SSCWeb system - SPDF (Goddard Space Flight Center)
GOLD_L2_NMAX: GOLD Peak Electron density NMAX L2 Daily Files - Richard Eastes (University of Colorado/LASP)
GOLD_L2_O2DEN: GOLD O2DEN L2 Daily Fileof O2 density - Richard Eastes (University of Colorado/LASP)
GOLD_L2_ON2: GOLD: O to N2 column ratio - Richard Eastes (University of Colorado/LASP)
GOLD_L2_TDISK: GOLD TDISK Neutral Temperatures - Richard Eastes (University of Colorado/LASP)
GPS_RF_LANL-VTEC-1HR: LANL Gridded Vertical Total Electron Content (VTEC)
GPS_ROTI15MIN_JPL: GPS-deduced ROTI index:standard deviation of rate of change of Total Electron Content (TEC) in a 15 min interval; world maps and movies - Xiaoqing Pi (Jet Propulsion Laboratory)
GPS_TEC15MIN_IGS: GPS-deduced 15-minute Total Electron Content (TEC) global maps and movies, UPC= U Politec. Catalonia Barcelona Spain - International Global Navigation Satellite Systems (GNSS) Service Iono Working Group
GPS_TEC1HR_IGS: GPS-deduced 1-hour Total Electron Content (TEC) global maps and movies, UPC= U Politec. Catalonia Barcelona Spain, ESA= ESOC Darmstadt Germany (starting 20 Feb 2011) - International Global Navigation Satellite Systems (GNSS) Service Ionosphere Working Group
GPS_TEC2HR_IGS: GPS-deduced 2-hour Total Electron Content (TEC) maps and movies, IGS= Average of 4 methods, incl. CODE= U Bern Switzerland, ESA= ESOC Darmstadt Germany, JPL= Jet Propulsion Lab. Pasadena USA, UPC= U Politec. Catalonia Barcelona Spain - International Global Navigation Satellite Systems (GNSS) Service Ionosphere Working Group
HALEBOPP_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HALEBOPP_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HALLEY_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HALLEY_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HEL1_6SEC_NESSMAG: HEL1_6SEC_NESSMAG - Mariani/Ness (University of Rome, CNR/Istituto Fisica Interplanetario, and NASA/GSFC)
HEL2_6SEC_NESSMAG: HEL2_6SEC_NESSMAG - Mariani/Ness (University of Rome, CNR/Istituto Fisica Interplanetario, and NASA/GSFC)
HELIOS1_40SEC_MAG-PLASMA: Merged 40.5 s magnetic field, plasma data, ephemeris - R. Schwenn, F. M. Neubauer (Max Planck Institute for Solar System Research, University of Cologne)
HELIOS1_COHO1HR_MERGED_MAG_PLASMA: Helios-1 merged hourly magnetic field, plasma, proton fluxes, and ephermis data - N. Ness, F. Neubauer, F. Mariani (magnetic field), H. Rosenbauer, R. Schwenn (plasma) and J. Freeman (all affiliated with ESA or NASA)
HELIOS1_E6_1HOUR_PARTICLE_FLUX: hourly averaged fluxes of e, H and He - H. Kunow (University of Kiel)
HELIOS1_E6_KUNOW_1HOUR_PARTICLE-FLUX: hourly averaged fluxes of e, H and He - H. Kunow (University of Kiel)
HELIOS1_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HELIOS1_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HELIOS2_40SEC_MAG-PLASMA: Merged 40.5 s magnetic field, plasma data, ephemeris - R. Schwenn, F. M. Neubauer (Max Planck Institute for Solar System Research, University of Cologne)
HELIOS2_COHO1HR_MERGED_MAG_PLASMA: Helios-2 merged hourly magnetic field, plasma, proton fluxes, and ephermis data - N. Ness, F. Neubauer, F. Mariani (magnetic field), H. Rosenbauer, R. Schwenn (plasma) and J. Freeman (all affiliated with ESA or NASA)
HELIOS2_E6_1HOUR_PARTICLE_FLUX: hourly averaged fluxes of e, H and He - H. Kunow (University of Kiel)
HELIOS2_E6_KUNOW_1HOUR_PARTICLE-FLUX: hourly averaged fluxes of e, H and He - H. Kunow (University of Kiel)
HELIOS2_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HELIOS2_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HK_H0_MAG: Hawkeye Magnetic Field Instrument - J. Van Allen (University of Iowa)
HK_H0_VLF: Hk Electric and Magnetic Field Radio Frequency Spectrum Analyzer High Time Resolution - D. Gurnett (University of Iowa)
HYAKUTAKE_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
HYAKUTAKE_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
I1_AV2_OTT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV2_QUI: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV2_SNT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV2_ULA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_ALL: ISIS-1 Topside sounder ionograms, all stations merged into a single dataset - R.F. Benson (NASA GSFC)
I1_AV_KER: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_KSH: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_KWA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_ODG: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_ORR: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_OTT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_QUI: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_RES: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_SNT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_SOD: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_TRO: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_ULA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_AV_WNK: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I1_NEPROF_TOPS: ISIS-1 CRC Electron Density Profiles - J. E. Jackson (Communication Research Centre (CRC), Ottawa)
I2_AV_ACN: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_ADL: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_AME: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_BRZ: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_BUR: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_CNA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_KER: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_KRU: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_KSH: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_KWA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_LAU: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_ODG: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_ORR: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_OTT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_QUI: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_RES: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_SNT: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_SOD: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_SOL: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_SYO: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_TRO: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_ULA: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_AV_WNK: ISIS Topside Sounder Ionogram - R.F. Benson (NASA GSFC)
I2_NEPROF_TOPIST: ISIS-2 TOPIST produced electron density profiles, of highest quality (quality flag = 2 and 3 - X. Huang and B. Reinisch (University of MassachusettsLowell)
I2_NEPROF_TOPS: ISIS-2 CRC Electron Density Profiles - J. E. Jackson (Communication Research Centre (CRC), Ottawa)
I7_R0_LEPEDEA: Link to IMP7 LEPEDEA Energy-Time Spectrograms in GIF format at the University of Iowa. - L. A. Frank (University of Iowa)
I8_15SEC_MAG: IMP-8 Fluxgate Magnetometer, 15.36-Second Resolution Data - A. Szabo / R.P. Lepping (NASA GSFC)
I8_320MSEC_MAG: IMP-8 Fluxgate Magnetometer, 320 msec Resolution Data - Adam Szabo, Joe King and Natalia Papitashvili (NASA GSFC)
I8_H0_GME: IMP-8 GME 30-min Fluxes (SEP optimal bands) - R.E. McGuire (SPDF (code632), NASA's GSFC)
I8_H0_MITPLASMA: IMP-8 MIT Plasma Investigation, High Resolution Definitive Data - A. Lazarus (MIT)
I8_OR_GIFWALK: Links to IMP-8 and multi-mission orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
I8_OR_SSC: IMP-8 orbital position (multiple coordinate systems, from April 2003 updated I8 orbit model) - SSC ( SPDF/GSFC)
I8_R0_LEPEDEA: Link to IMP8 LEPEDEA Energy-Time Spectrograms in GIF format at the University of Iowa. - L. A. Frank (University of Iowa)
IA_K0_ENF: Interball Auroral Probemeasurements of spectra and anisotropy of electrons SKA-3, Key Parameters - Yu. Galperin, R. Kovrazhkin, A. Kuzmin, F. Shuiskaya (IKI RAN, Russia)
IA_K0_EPI: Interball Auroral Energetic Particle Instruments, Key Parameters - DOK-2: K.Kudela (DOK-2: Institute of experimental physics Slovak Acad. Sci., Kosize, Slovakia )
IA_K0_ICD: Interball Auroral Probe Ion Composition Experiment PROMICS, Key Parameters - I.Sandahl (IRF, Kiruna, Sweden)
IA_K0_MFI: Interball Auroral probe Magnetic Field, Key Parameters - V.Petrov (IZMIRAN,Troitsk, Russia. )
IA_OR_DEF: Interball Tail Orbital Data, Key Parameters - V.Prokhorenko (Space Research Inst., Russian Acad. Sci., Moscow, Russia. )
IBEX_H3_ENA_HI_R02_CG_NOSP_OMNI_6MO: IBEX-Hi Release 2; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R02_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release 2; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 4; Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_NOSP_OMNI_6MO: IBEX-Hi Release 4; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_NOSP_RAM_1YR: IBEX-Hi Release 4; Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_SP_ANTIRAM_1YR: IBEX-Hi Release 4; Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_SP_OMNI_6MO: IBEX-Hi Release 4; Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_CG_SP_RAM_1YR: IBEX-Hi Release 4; Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_DEFLECTION_1AU_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_DEFLECTION_SCF_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_LOSS_1AU_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_LOSS_SCF_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 4; no Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_3YR: IBEX-Hi Release 4; no Compton-Getting, no Survival-Probability, omni-direction 3-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release 4; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_6MP: IBEX-Hi Release 4; no Compton-Getting, no Survival-Probability, omni-direction 3-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_NOSP_RAM_1YR: IBEX-Hi Release 4; no Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_SP_ANTIRAM_1YR: IBEX-Hi Release 4; no Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_SP_OMNI_6MO: IBEX-Hi Release 4; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_NOCG_SP_RAM_1YR: IBEX-Hi Release 4; no Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_SURVPRO_1AU_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R04_SURVPRO_SCF_7DAY: IBEX-Hi Release 4; Survival Probabilities tables - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_ANTIRAM_MIF_5YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_ANTIRAM_VEIF_5YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_6MO: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_MIF_10MP: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_VEIF_10MP: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_1YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_MIF_5YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_VEIF_5YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_1YR: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_MIF_5YR: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_VEIF_5YR: IBEX-Hi Release 7; Compton-Getting, no Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_OMNI_6MO: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_OMNI_MIF_10MP: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Omnidirectional 1-to-10 map Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_OMNI_VEIF_10MP: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_RAM_1YR: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_RAM_MIF_5YR: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Mono Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_CG_SP_RAM_VEIF_5YR: IBEX-Hi Release 7; Compton-Getting, Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_ANTIRAM_VESCF_5YR: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_OMNI_VESCF_10MP: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_RAM_1YR: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_NOSP_RAM_VEIF_5YR: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy Inertial Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_ANTIRAM_1YR: IBEX-Hi Release 7; no Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_ANTIRAM_VESCF_5YR: IBEX-Hi Release 7; no Compton-Getting, no Survival-Probability, Antiram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_OMNI_6MO: IBEX-Hi Release 7; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_OMNI_VESCF_10MP: IBEX-Hi Release 7; no Compton-Getting, Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_RAM_1YR: IBEX-Hi Release 7; no Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R07_NOCG_SP_RAM_VESCF_5YR: IBEX-Hi Release 7; no Compton-Getting, Survival-Probability, Ram-directional 1-to-5-year Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS-GAL_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS-J2000_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS-GALACTIC_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS-J2000_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS_5YR: IBEX-Hi Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_ANTIRAM_1YR: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, antiram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_ANTIRAM_7YR: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, antiram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_OMNI_6MO: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_OMNI_7YR: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, omni-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_RAM_1YR: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, ram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_NOSP_RAM_7YR: IBEX-Hi Release-10; Compton-Getting, no Survival-Probability, ram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_ANTIRAM_1YR: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, AntiRAMdirectional 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_ANTIRAM_7YR: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, antiram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_OMNI_6MO: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_OMNI_7YR: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, omni-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_RAM_1YR: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, RAMdirectional 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_CG_SP_RAM_7YR: IBEX-Hi Release-10; Compton-Getting, Survival-Probability, ram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_NOSP_ANTIRAM_1YR: IBEX-Hi Release-10; no Compton-Getting, no Survival-Probability, antiram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_NOSP_ANTIRAM_7YR: IBEX-Hi Release-10; no Compton-Getting, no Survival-Probability, antiram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release-10; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_NOSP_OMNI_7YR: IBEX-Hi Release-10; no Compton-Getting, no Survival-Probability, omni-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_NOSP_RAM_1YR: IBEX-Hi Release-10; no Compton-Getting, no Survival-Probability, ram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_SP_ANTIRAM_1YR: IBEX-Hi Release-10; no Compton-Getting, Survival-Probability, antiram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_SP_ANTIRAM_7YR: IBEX-Hi Release-10; no Compton-Getting, Survival-Probability, antiram-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_SP_OMNI_6MO: IBEX-Hi Release-10; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_SP_OMNI_7YR: IBEX-Hi Release-10; no Compton-Getting, Survival-Probability, omni-direction 7-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R10_NOCG_SP_RAM_1YR: IBEX-Hi Release-10; no Compton-Getting, Survival-Probability, ram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R12_MAGNETOSPHERE_24MIN: IBEX-Hi Release-12; Count Data for Magnetospheric Imaging. - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R13_CG_NOSP_ANTIRAM_1YR: IBEX-Hi Release-13; Compton-Getting, no Survival-Probability, antiram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R13_CG_NOSP_RAM_1YR: IBEX-Hi Release-13; Compton-Getting, no Survival-Probability, ram-direction 1-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R14_PRESS-SLOPE_CG_NOSP_RAM_3YR: IBEX-Hi Release-14; Compton-Getting, no Survival-Probability, ram-direction 3-year-Average West Ecliptic Pressure andFlux Power-Law Slope Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_1YR: IBEX-Hi Release 15; Compton-Getting, Survival-Probability, in a ribbon centered frame, 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_2YR: IBEX-Hi Release 15; Compton-Getting, Survival-Probability, in a ribbon centered frame, 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_3YR: IBEX-Hi Release 15; Compton-Getting, Survival-Probability, in a ribbon centered frame, 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, ANTIRAMdirectional 11-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, ANTIRAMdirectional mono-energy 11-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_MONO_1YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, ANTIRAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Omnidirectional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_6MO: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Omnidirectional, mono-energy 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_MONO_6MO: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Omnidirectional, mono-energy 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, ram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_1YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, RAMdirectional mono-energy 11-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_MONO_1YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, RAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Antiram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_1YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, ANTIRAMdirectional, mono-energy 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_MONO_1YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, ANTIRAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_11YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_2YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional 2-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_3YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional 2-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_6MO: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional, mono-energy 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_OMNI_MONO_6MO: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, Omnidirectional, mono-energy 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_RAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Ram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_RAM_1YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_RAM_MONO_11YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, RAMdirectional, mono-energy 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_CG_SP_RAM_MONO_1YR: IBEX-Hi Release 16; Compton-Getting, Survival-Probability, RAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_ANTIRAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Antiram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 16; no Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_OMNI_11YR: IBEX-Hi Release 16; no Compton-Getting, no Survival-Probability, Omnidirectional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release 16; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_RAM_11YR: IBEX-Hi Release 16; Compton-Getting, no Survival-Probability, Ram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_NOSP_RAM_1YR: IBEX-Hi Release 16; no Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_ANTIRAM_11YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Antiram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_ANTIRAM_1YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_OMNI_11YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Omnidirectional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_OMNI_6MO: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_RAM_11YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Ram-directional 11-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_RAM_1YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_RAM_EQUA_11YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Ram-directional 11-year-Average West Ecliptic Maps in Equatorial coordinates - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R16_NOCG_SP_RAM_GALA_11YR: IBEX-Hi Release 16; no Compton-Getting, Survival-Probability, Ram-directional 11-year-Average West Maps in Galactic coordinates - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_ANTIRAM_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, Antiram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, Antiramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_ANTIRAM_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, ANTIRAMdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_ANTIRAM_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, ANTIRAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_OMNI_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, omni-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_OMNI_6MO: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_OMNI_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, OMNIdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_OMNI_MONO_6MO: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, Omnidirectional mono-energy 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_RAM_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_RAM_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, Ramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_RAM_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, RAMdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_NOSP_RAM_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, RAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_LOWER_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional lower gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_LOWER_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional lower gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_LOWER_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional lower ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_LOWER_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional lower ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MEDIAN_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional median gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MEDIAN_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional median gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MEDIAN_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional median ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MEDIAN_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional median ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ANTIRAMdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, ANTIRAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_UPPER_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional upper gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_UPPER_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional upper gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_UPPER_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional upper ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_ANTIRAM_UPPER_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Antiramdirectional upper ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_OMNI_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, omni-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_OMNI_6MO: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_OMNI_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, OMNIdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_OMNI_MONO_6MO: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Omnidirectional mono-energy 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_LOWER_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional lower gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_LOWER_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ramdirectional lower gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_LOWER_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional lower ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_LOWER_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ramdirectional lower ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MEDIAN_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional median gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MEDIAN_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ramdirectional median gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MEDIAN_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional median ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MEDIAN_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, ramdirectional median ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MONO_14YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, RAMdirectional mono-energy 14-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, no Survival-Probability, RAMdirectional mono-energy 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_UPPER_GDF_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional upper gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_UPPER_GDF_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional upper gdf mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_UPPER_RIBBON_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional upper ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_CG_SP_RAM_UPPER_RIBBON_MONO_1YR: IBEX-Hi Release 18; Compton-Getting, Survival-Probability, Ramdirectional upper ribbon mono-energy 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_ANTIRAM_14YR: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, Antiram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_ANTIRAM_1YR: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, Antiramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_OMNI_14YR: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, omni-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_OMNI_6MO: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_RAM_14YR: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_NOSP_RAM_1YR: IBEX-Hi Release 18; no Compton-Getting, no Survival-Probability, Ramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_14YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_LOWER_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional lower gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_LOWER_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional lower ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_MEDIAN_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional median gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_MEDIAN_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional median ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_UPPER_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional upper gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_ANTIRAM_UPPER_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Antiramdirectional upper ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_OMNI_14YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, omni-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_OMNI_6MO: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_14YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_EQUA_14YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps in Equatorial coordinates - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_GALA_14YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, ram-directional 14-year-Average West Ecliptic Maps in galactic coordinates - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_LOWER_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional lower gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_LOWER_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional lower ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_MEDIAN_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional median gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_MEDIAN_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional median ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_UPPER_GDF_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional upper gdf 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_HI_R18_NOCG_SP_RAM_UPPER_RIBBON_1YR: IBEX-Hi Release 18; no Compton-Getting, Survival-Probability, Ramdirectional upper ribbon 1-year-average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R03_ANGULAR_ANALYSIS_7DAY: IBEX-Hi Release 3; Angular analysis - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R03_CT_RATE_ANALYSIS_7DAY: IBEX-Hi Release 3; Count Rate analysis - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R04_CG_SP_ANTIRAM_3YR: IBEX-Lo Release 4; Compton-Getting, Survival-Probability, ANTIRAM direction, 3-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R04_CG_SP_RAM_3YR: IBEX-Lo Release 4; Compton-Getting, Survival-Probability, RAM-directional 3-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R06_SCHWADRON-H: IBEX-Hi Release 6; Count Data for Heliospheric Imaging. - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R06_SCHWADRON-HE: IBEX-Lo Release 6; Count Data for Heliospheric Imaging. - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R06_STATE_VECTORS: IBEX State Vectors - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R07_NOCG_NOSP_OMNI_6MO: IBEX-Lo Release-07; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R07_NOCG_NOSP_OMNI_VESCF_10MP: IBEX-Lo Release 7; no Compton-Getting, no Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R07_NOCG_SP_OMNI_6MO: IBEX-Lo Release-07; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R07_NOCG_SP_OMNI_VESCF_10MP: IBEX-Lo Release 7; no Compton-Getting, Survival-Probability, Omnidirectional 1-to-10-map Average West Ecliptic Maps in Var Energy SC Frame - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F2-RIBBON-MAPS-GAL_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F2-RIBBON-MAPS-J2000_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F2-RIBBON-MAPS_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F3-GDF-MAPS-GALACTIC_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F3-GDF-MAPS-J2000_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R08_OMNI_F3-GDF-MAPS_5YR: IBEX-Lo Release-08; omni-direction 5-year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_HEIRTZLER-H_7DAY: IBEX Release-9; IBEX-Lo Interstellar Neutral Histogram Counts and Direct Event Counts - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_PARK_OMAP_3YR: IBEX-Lo Release-09; Park et al. 2015) 3-year combined heavy neutral maps: m1-to-m6 (map1 + map2 + map3 + map4 + map5 + map6) West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_PARK_OMAP_3YR-EVEN-MAPS: IBEX-Lo Release-09; Park et al. 2015) 3-year combined heavy neutral even maps: m2m4m6 (map2 + map4 + map6) West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_PARK_OMAP_3YR-ODD-MAPS: IBEX-Lo Release-09; Park et al. 2015) 3-year combined heavy neutral odd maps: m1m3m5 (map1 + map3 + map5) West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_PARK_OMAP_6MO: IBEX-Lo Release-09; Park Oxygen Map Counting Rate 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_PARK_OMAP_STAT_3YR: IBEX-Lo Release-09; Park et al. (2015) 3-year combined heavy neutral maps: m1-to-m6 (map1 + map2 + map3 + map4 + map5 + map6) with statistical filtering - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R09_SCHWADRON-INTERSTELLAR-HE_1YR: IBEX Release-9; Interstellar He Parameters - David McComas (Princeton University)
IBEX_H3_ENA_LO_R10_NOCG_NOSP_OMNI_6MO: IBEX-Lo Release-10; no Compton-Getting, no Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R10_NOCG_NOSP_OMNI_7YR: IBEX-Lo Release-10; no Compton-Getting, no Survival-Probability, Omnidirectional 7-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R10_NOCG_SP_OMNI_6MO: IBEX-Lo Release-10; no Compton-Getting, Survival-Probability, Omnidirectional 6-month-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R10_NOCG_SP_OMNI_7YR: IBEX-Lo Release-10; no Compton-Getting, Survival-Probability, Omnidirectional 7-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R11_SCHWADRON-INTERSTELLAR-O: IBEX Release-11; Oxygen count rates for different spin phase bins organized by orbit - David McComas (Southwest Research Institute, San Antonio, TX)
IBEX_H3_ENA_LO_R17_CG_NOSP_ANTIRAM_1YR: IBEX-lo Release 17; Compton-Getting, no Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_CG_NOSP_OMNI_1YR: IBEX-lo Release 17; Compton-Getting, no Survival-Probability, OMNIdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_CG_NOSP_RAM_1YR: IBEX-lo Release 17; Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_CG_SP_ANTIRAM_1YR: IBEX-lo Release 17; Compton-Getting, Survival-Probability, ANTIRAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_CG_SP_OMNI_1YR: IBEX-lo Release 17; Compton-Getting, no Survival-Probability, OMNIdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_CG_SP_RAM_1YR: IBEX-lo Release 17; Compton-Getting, Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_LO_R17_NOCG_NOSP_RAM_1YR: IBEX-lo Release 17; no Compton-Getting, no Survival-Probability, RAMdirectional 1-Year-Average West Ecliptic Maps - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_R05_MARINER-H-HE: IBEX Data Release 5 - Mariner 10 Hydrogen Ly-alpha backscattered emision and Helium 584A backscattered solar emission from Roll Control Maneuver #7 of Mariner 10. - Dr. David J. McComas (Princeton University)
IBEX_H3_ENA_R18_STATE_VECTOR: IBEX State Vectors - Dr. David J. McComas (Princeton University)
IBEX_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
ICON_L2-1_MIGHTI-A_LOS-WIND-GREEN: Michelson Interferometer for Global High-resolution Thermospheric Imaging (MIGHTI) Sensor A: Line-of-sight Wind Profiles - T. J. Immel (UC Berkeley>SSL)
ICON_L2-1_MIGHTI-A_LOS-WIND-RED: Michelson Interferometer for Global High-resolution Thermospheric Imaging (MIGHTI) Sensor A: Line-of-sight Wind Profiles - T. J. Immel (UC Berkeley>SSL)
ICON_L2-1_MIGHTI-B_LOS-WIND-GREEN: Michelson Interferometer for Global High-resolution Thermospheric Imaging (MIGHTI) Sensor B - Line-of-sight Wind Profiles - T. J. Immel (UC Berkeley>SSL)
ICON_L2-1_MIGHTI-B_LOS-WIND-RED: Michelson Interferometer for Global High-resolution Thermospheric Imaging (MIGHTI) Sensor B - Line-of-sight Wind Profiles - T. J. Immel (UC Berkeley>SSL)
ICON_L2-2_MIGHTI_VECTOR-WIND-GREEN: MIGHTI - Cardinal Vector Winds - T. J. Immel (UC Berkeley>SSL)
ICON_L2-2_MIGHTI_VECTOR-WIND-RED: MIGHTI - Cardinal Vector Winds - T. J. Immel (UC Berkeley>SSL)
ICON_L2-3_MIGHTI-A_TEMPERATURE: ICON MIGHTI-A Level 2.3 Retrieved Temperature File - T. J. Immel (UC Berkeley>SSL)
ICON_L2-3_MIGHTI-B_TEMPERATURE: ICON MIGHTI-B Level 2.3 Retrieved Temperature File - T. J. Immel (UC Berkeley>SSL)
ICON_L2-4_FUV_DAY: ICON FUV Daytime: column density ratio of thermospheric atomic oxygen to molecular nitrogen. - T. J. Immel (UC Berkeley>SSL)
ICON_L2-4_FUV_DAY-LIMB: ICON FUV Daytime Limb - T. J. Immel (UC Berkeley > SSL)
ICON_L2-5_FUV_NIGHT: FUV Short Wavelength Channel - 135.6 Altitude Profiles (night) - T. J. Immel (UC Berkeley>SSL)
ICON_L2-6_EUV: ICON EUV derived ionospheric data products - T. J. Immel (UC Berkeley>SSL)
ICON_L2-7_IVM-A: ICON Ion Velocity Meter (IVM) Thermal Plasma Measurements
ICON_L2-7_IVM-B: ICON IVM Thermal Plasma Measurements B - T. J. Immel (UC Berkeley>SSL)
IG_K0_PCI: Interball Polar Cap Activity Index, Key Parameters - V.Sergeev (Institute of physics Univ. of St.-Peterburg St.-Peterburg, Russia )
IMAGE_M2_EUV: Imager for Magnetospause-to-Aurora Global Extreme Ultraviolet Imager Modified Data 2 - R. M. Katus (Eastern Michigan University)
IM_ELECTRON_DENSITY_RPI: RPI Dynamic Spectrogram, Electron Plasma, IMAGE Radio Plasma Imager (RPI) - B.W. Reinisch (UMLCAR)
IM_HK_ADS: Image Attitude Determination System Housekeeping - Dr. Jim Burch (Southwest Research Institute)
IM_HK_AST: Image Autonomous Star Tracker Housekeeping - Dr. Jim Burch (Southwest Research Institute)
IM_HK_COM: Image Communication Systems Housekeeping - Dr. Jim Burch (Southwest Research Institute)
IM_HK_FSW: IMAGE FSW - Dr. Jim Burch (Southwest Research Institute)
IM_HK_PWR: Image Power Systems Housekeeping - Dr. Jim Burch (Southwest Research Institute)
IM_HK_TML: Image Thermal Housekeeping - Dr. Jim Burch (Southwest Research Institute)
IM_K0_EUV: Ion Images, Key Parameters, IMAGE Extreme UltraViolet (EUV) experiment - W. Sandel (U/Arizona)
IM_K0_HENA: Image HIGH ENERGY NEUTRAL ATOM IMAGER Key Parameter - Dr. Don Mitchell (APL)
IM_K0_LENA: Image LOW ENERGY NEUTRAL ATOM IMAGER Key Parameter - Dr. Tom Moore (GSFC)
IM_K0_MENA: Image MEDIUM ENERGY NEUTRAL ATOM IMAGER Key Parameter - Dr. Craig Pollock (SwRI)
IM_K0_RPI: RPI Plasmagram/Echomap, Key Parameters, IMAGE Radio Plasma Imager (RPI) - B.W. Reinisch (UMLCAR)
IM_K0_SIE: Image Spectrographic Imaging Camera Key parameter - S. Mende (UC/Berkeley/SSL)
IM_K0_SIP: Image Spectrographic Imaging Camera Key parameter - S. Mende (UC/Berkeley/SSL)
IM_K0_WIC: Image Wide-Band Imaging Camera Key parameter - S. Mende (UC/Berkeley/SSL)
IM_K1_RPI: RPI Dynamic Spectrogram, Key Parameters, IMAGE Radio Plasma Imager (RPI) - B.W. Reinisch (UMLCAR)
IM_OR_DEF: IMAGE Definitive Orbit - Dr. Jim Burch (Southwest Research Institute)
IM_OR_GIFWALK: Link to IMAGE orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
IM_OR_PRE: IMAGE Predicted Orbit - Dr. Jim Burch (Southwest Research Institute)
ISEE-3_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
ISEE-3_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
ISEE-3_MAGPLASMA_2MIN_MAGNETIC_FIELD_PLASMA: 2 min averaged magnetic field and plasma - Edward Smith (JPL NASA)
ISEE-3_MAG_1MIN_MAGNETIC_FIELD: 1 min averaged magnetic field - Edward Smith (JPL NASA)
ISEE1_4SEC_MFI: 12-sec avg vector magnetic field at 4-sec intervals - C. T. Russell (UCLA)
ISEE1_60SEC_MFI: 60-sec vector magnetic field - C. T. Russell (UCLA)
ISEE1_H0_FE: ISEE1_Fast Electrons - K. Ogilvie (GSFC Code 690)
ISEE1_H1_FPE: ISEE 1_H1_FPE / Proton Fluid Parameters 6 RE - Bow Shock - S. Bame & J. Gosling (LANL)
ISEE1_H2_FPE: ISEE 1_H2_FPE / Solar Wind 24-sec Ion Moments - S. Bame & J. Gosling (LANL)
ISEE1_PWI_SA: ISEE-1 PWI: Spectrum Analyzer (SA) - Donald Gurnett (University Iowa)
ISEE1_PWI_SA-RAPID-E: ISEE-1 PWI: Spectrum Analyzer (SA) rapid samples - Donald Gurnett (University Iowa)
ISEE1_PWI_SFR-E: ISEE-1 PWI: Sweep Frequency Receiver (SFR) - Donald Gurnett (University Iowa)
ISEE2_4SEC_MFI: 12-sec avg vector magnetic field at 4-sec intervals - C. T. Russell (UCLA)
ISEE2_60SEC_MFI: 60-sec vector magnetic field - C. T. Russell (UCLA)
ISEE2_H1_FPE: ISEE 2_H1_FPE / Proton Fluid Parameters 6 RE - Bow Shock - G. Paschmann (MPE)
ISS_27DAY-AVERAGES_AMS-02: AMS-02 proton flux (p), helium flux (He), p/He flux ratio, electron flux (e-), positron flux (e+) and e+/e- flux ratio at Bartels rotation time resolution - Prof. V. Bindi (University of Hawaii at Manoa)
ISS_DOSANL_TEPC: Experiment Data, ISS TEPC (from ASCII DOS.TXT file) - Edward Semones (NASA Space Radiation Analysis Group/Johnson Space Center)
ISS_SP_FPMU: ISS FPMU 1-sec Summary Plasma Densities, Temperatures, Spacecraft Potentials. - E. Willis (NASA Marshall Space Flight Center)
IT_H0_MFI: Interball-Tail 6 sec vector magnetic field data - M.Nozdrachev (IKI, Moscow, Russia)
IT_K0_AKR: Interball Tail Probe AKR Radioemission flux, Key Parameters - V.Kurilchik (Sternberg Astronomical Inst.,Moscow State University, 119899, Universitetsky pr., 13 Moscow, Russia)
IT_K0_COR: Interball Tail Probe CORALL ion moments, Key Parameters - Yu.Yermolaev (Space Research Inst., Russian Acad. Sci., Moscow, Russia)
IT_K0_ELE: Interball Tail probe ELECTRON instrument, Key Parameters - J.-A. Sauvaud (CESR, BP 4346, 31029, Toulouse, France )
IT_K0_EPI: Interball Tail Energetic Particle Instruments, Key Parameters - DOK-2: K.Kudela (DOK-2: Institute of experimental physics Slovak Acad. Sci., Kosize, Slovakia )
IT_K0_ICD: Interball Tail Probe Ion Composition Experiment PROMICS, Key Parameters - I.Sandahl (IRF, Kiruna, Sweden)
IT_K0_MFI: Interball Tail probe Magnetic Field, Key Parameters - S.Romanov (Space Research Inst., Russian Acad. Sci., Moscow, Russia. )
IT_K0_VDP: Interball Tail probe VDP instrument, Key Parameters - J.Safrankova (Charles University, Prague, Czech Republic )
IT_K0_WAV: Interball Tail probe Magnetic Field, Key Parameters - S.Romanov (Space Research Inst., Russian Acad. Sci., Moscow, Russia. )
IT_OR_DEF: Interball Tail Orbital Data, Key Parameters - V.Prokhorenko (Space Research Inst., Russian Acad. Sci., Moscow, Russia. )
IT_OR_GIFWALK: Links to Interball-Tail and multi-mission orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
JUNO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
JUNO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
JUPITER_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
JUPITER_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
L0_K0_MPA: LANL 1990-095 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
L0_K0_SPA: LANL 1990 Synchronous Orbit Particle Analyzer Key Parameters - Reiner Friedel (LANL)
L1_K0_GIFWALK: Links to GEOSYNC KP pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
L1_K0_MPA: LANL 1991-080 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
L1_K0_SPA: LANL 1991 Synchronous Orbit Particle Analyzer Key Parameters - Reiner Friedel (LANL)
L4_K0_MPA: LANL 1994-084 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
L4_K0_SPA: LANL 1994 Synchronous Orbit Particle Analyzer Key Parameters - Reiner Friedel (LANL)
L7_H0_MPA: LANL 1997 Magnetospheric Plasma Analyzer High Resolution data - D. McComas (LANL)
L7_K0_MPA: LANL 1997 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
L7_K0_SPA: LANL 1997 Synchronous Orbit Particle Analyzer Key Parameters - Reiner Friedel (LANL)
L9_H0_MPA: LANL 1989-046 Magnetospheric Plasma Analyzer High Resolution data - D. McComas (LANL)
L9_K0_MPA: LANL 1989-046 Magnetospheric Plasma Analyzer Key Parameters - D. McComas (LANL)
L9_K0_SPA: LANL 1989 Synchronous Orbit Particle Analyzer Key Parameters - Reiner Friedel (LANL)
MARINER2_R0_MAGPLASMA: Mariner2 merged magnetic field and plasma hourly data from COHOWeb Service
MARS_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MARS_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MAVEN_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MAVEN_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MERCURY_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MERCURY_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MESSENGER_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MESSENGER_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MESSENGER_MAG_RTN: MESSENGER interplanetary magnetic field (1-second/high resolution) in RTN coordinates - Prof. Sean C. Solomon (Carnegie Institution of Washington)
METOP1_POES-SEM2_FLUXES-2SEC: POES-SEM2 2-second Particle Precipitation Data, MetOp-B (MetOp-1 before Sept2012 launch) [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
METOP2_POES-SEM2_FLUXES-2SEC: POES-SEM2 2-second Particle Precipitation Data, MetOp-A (MetOp-2 before Oct2006 launch) [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
METOP3_POES-SEM2_FLUXES-2SEC: POES-SEM2 2-second Particle Precipitation Data, MetOp-C (MetOp-3 launched 07 November 2018) [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NCEI (NOAA)
MGS_MAG_HIGH: Mars Global Surveyor Magnetometer High Resolution - M. Acuna (NASA/GSFC)
MGS_MAG_LOW: Mars Global Surveyor Magnetometer Modified Data - M. Acuna (NASA/GSFC)
MMS1_ASPOC_SRVY_L2: Level 2 Active Spacecraft Potential Control Survey Data - K. Torkar, R. Nakamura (IWF)
MMS1_DSP_FAST_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS1_DSP_FAST_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS1_DSP_SLOW_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS1_DSP_SLOW_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS1_EDI_BRST_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS1_EDI_BRST_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS1_EDI_BRST_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS1_EDI_BRST_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS1_EDI_SRVY_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS1_EDI_SRVY_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS1_EDI_SRVY_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS1_EDI_SRVY_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS1_EDP_BRST_L2_DCE: MMS1 L2 (brst), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_BRST_L2_HMFE: MMS1 l2 (brst), 3D HMFE Electric field - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS1_EDP_BRST_L2_SCPOT: MMS 1 dual probe scpot (brst), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_FAST_L2_DCE: MMS1 L2 (fast), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_FAST_L2_SCPOT: MMS 1 dual probe scpot (fast), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_SLOW_L2_DCE: MMS1 L2 (slow), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_SLOW_L2_SCPOT: MMS 1 dual probe scpot (slow), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS1_EDP_SRVY_L2_HFESP: MMS1 L2 (srvy), HF ACE Spectra - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS1_EPD-EIS_BRST_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Brst - B. Mauk (JHU/APL)
MMS1_EPD-EIS_BRST_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Brst - B. Mauk (JHU/APL)
MMS1_EPD-EIS_SRVY_L2_ELECTRONENERGY: Level 2 Energetic Ion Spectrometer Electron Spectra Srvy - B. Mauk (JHU/APL)
MMS1_EPD-EIS_SRVY_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Srvy - B. Mauk (JHU/APL)
MMS1_EPD-EIS_SRVY_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Srvy - B. Mauk (JHU/APL)
MMS1_FEEPS_BRST_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS1_FEEPS_BRST_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS1_FEEPS_SRVY_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS1_FEEPS_SRVY_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS1_FGM_BRST_L2: Level2 Flux Gate Magnetometer Burst DC Magnetic Field for MMS Satellite Number 1 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS1_FGM_SRVY_L2: Level2 Flux Gate Magnetometer Combined Fast/Slow Survey DC Magnetic Field for MMS Satellite Number 1 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS1_FPI_BRST_L2_DES-DIST: MMS Satellite Number 1 Dual Electron Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_BRST_L2_DES-MOMS: MMS Satellite Number 1 Dual Electron Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_BRST_L2_DES-PARTMOMS: MMS Satellite Number 1 Dual Electron Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_BRST_L2_DIS-DIST: MMS Satellite Number 1 Dual Ion Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_BRST_L2_DIS-MOMS: MMS Satellite Number 1 Dual Ion Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_BRST_L2_DIS-PARTMOMS: MMS Satellite Number 1 Dual Ion Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DES-DIST: MMS Satellite Number 1 Dual Electron Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DES-MOMS: MMS Satellite Number 1 Dual Electron Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DES-PARTMOMS: MMS Satellite Number 1 Dual Electron Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DIS-DIST: MMS Satellite Number 1 Dual Ion Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DIS-MOMS: MMS Satellite Number 1 Dual Ion Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_FPI_FAST_L2_DIS-PARTMOMS: MMS Satellite Number 1 Dual Ion Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS1_HPCA_BRST_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS1_HPCA_BRST_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS1_HPCA_SRVY_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS1_HPCA_SRVY_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS1_HPCA_SRVY_L2_TOF-COUNTS: Level 1b> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS1_MEC_BRST_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_MEC_BRST_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_MEC_BRST_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_MEC_SRVY_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_MEC_SRVY_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_MEC_SRVY_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 1 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS1_R0_SUMMARY: Links to MMS-1 pre-generated Quicklook Summary plots - James Burch (SWRI)
MMS1_SCM_BRST_L2_SCB: Level 2 Search Coil Magnetometer AC Magnetic Field Burst (8192S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS1_SCM_BRST_L2_SCHB: Level 2 Search Coil Magnetometer AC Magnetic Field High Burst (16384S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS1_SCM_SRVY_L2_SCSRVY: Level 2 Search Coil Magnetometer AC Magnetic Field Survey (32S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS2_ASPOC_SRVY_L2: Level 2 Active Spacecraft Potential Control Survey Data - K. Torkar, R. Nakamura (IWF)
MMS2_DSP_FAST_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS2_DSP_FAST_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS2_DSP_SLOW_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS2_DSP_SLOW_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS2_EDI_BRST_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS2_EDI_BRST_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS2_EDI_BRST_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS2_EDI_BRST_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS2_EDI_SRVY_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS2_EDI_SRVY_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS2_EDI_SRVY_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS2_EDI_SRVY_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS2_EDP_BRST_L2_DCE: MMS2 L2 (brst), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_BRST_L2_HMFE: MMS2 l2 (brst), 3D HMFE Electric field - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS2_EDP_BRST_L2_SCPOT: MMS 2 dual probe scpot (brst), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_FAST_L2_DCE: MMS2 L2 (fast), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_FAST_L2_SCPOT: MMS 2 dual probe scpot (fast), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_SLOW_L2_DCE: MMS2 L2 (slow), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_SLOW_L2_SCPOT: MMS 2 dual probe scpot (slow), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS2_EDP_SRVY_L2_HFESP: MMS2 L2 (srvy), HF ACE Spectra - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS2_EPD-EIS_BRST_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Brst - B. Mauk (JHU/APL)
MMS2_EPD-EIS_BRST_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Brst - B. Mauk (JHU/APL)
MMS2_EPD-EIS_SRVY_L2_ELECTRONENERGY: Level 2 Energetic Ion Spectrometer Electron Spectra Srvy - B. Mauk (JHU/APL)
MMS2_EPD-EIS_SRVY_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Srvy - B. Mauk (JHU/APL)
MMS2_EPD-EIS_SRVY_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Srvy - B. Mauk (JHU/APL)
MMS2_FEEPS_BRST_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS2_FEEPS_BRST_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS2_FEEPS_SRVY_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS2_FEEPS_SRVY_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS2_FGM_BRST_L2: Level2 Flux Gate Magnetometer Burst DC Magnetic Field for MMS Satellite Number 2 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS2_FGM_SRVY_L2: Level2 Flux Gate Magnetometer Combined Fast/Slow Survey DC Magnetic Field for MMS Satellite Number 2 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS2_FPI_BRST_L2_DES-DIST: MMS Satellite Number 2 Dual Electron Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_BRST_L2_DES-MOMS: MMS Satellite Number 2 Dual Electron Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_BRST_L2_DES-PARTMOMS: MMS Satellite Number 2 Dual Electron Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_BRST_L2_DIS-DIST: MMS Satellite Number 2 Dual Ion Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_BRST_L2_DIS-MOMS: MMS Satellite Number 2 Dual Ion Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_BRST_L2_DIS-PARTMOMS: MMS Satellite Number 2 Dual Ion Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DES-DIST: MMS Satellite Number 2 Dual Electron Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DES-MOMS: MMS Satellite Number 2 Dual Electron Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DES-PARTMOMS: MMS Satellite Number 2 Dual Electron Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DIS-DIST: MMS Satellite Number 2 Dual Ion Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DIS-MOMS: MMS Satellite Number 2 Dual Ion Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_FPI_FAST_L2_DIS-PARTMOMS: MMS Satellite Number 2 Dual Ion Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS2_HPCA_BRST_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS2_HPCA_BRST_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS2_HPCA_SRVY_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS2_HPCA_SRVY_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS2_HPCA_SRVY_L2_TOF-COUNTS: Level 1b> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS2_MEC_BRST_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_MEC_BRST_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_MEC_BRST_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_MEC_SRVY_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_MEC_SRVY_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_MEC_SRVY_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 2 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS2_R0_SUMMARY: Links to MMS-2 pre-generated Quicklook Summary plots - James Burch (SWRI)
MMS2_SCM_BRST_L2_SCB: Level 2 Search Coil Magnetometer AC Magnetic Field Burst (8192S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS2_SCM_BRST_L2_SCHB: Level 2 Search Coil Magnetometer AC Magnetic Field High Burst (16384S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS2_SCM_SRVY_L2_SCSRVY: Level 2 Search Coil Magnetometer AC Magnetic Field Survey (32S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS3_ASPOC_SRVY_L2: Level 2 Active Spacecraft Potential Control Survey Data - K. Torkar, R. Nakamura (IWF)
MMS3_DSP_FAST_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS3_DSP_FAST_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS3_DSP_SLOW_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS3_DSP_SLOW_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS3_EDI_BRST_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS3_EDI_BRST_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS3_EDI_BRST_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS3_EDI_BRST_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS3_EDI_SRVY_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS3_EDI_SRVY_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS3_EDI_SRVY_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS3_EDI_SRVY_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS3_EDP_BRST_L2_DCE: MMS3 L2 (brst), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_BRST_L2_HMFE: MMS3 l2 (brst), 3D HMFE Electric field - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS3_EDP_BRST_L2_SCPOT: MMS 3 dual probe scpot (brst), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_FAST_L2_DCE: MMS3 L2 (fast), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_FAST_L2_SCPOT: MMS 3 dual probe scpot (fast), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_SLOW_L2_DCE: MMS3 L2 (slow), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_SLOW_L2_SCPOT: MMS 3 dual probe scpot (slow), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS3_EDP_SRVY_L2_HFESP: MMS3 L2 (srvy), HF ACE Spectra - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS3_EPD-EIS_BRST_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Brst - B. Mauk (JHU/APL)
MMS3_EPD-EIS_BRST_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Brst - B. Mauk (JHU/APL)
MMS3_EPD-EIS_SRVY_L2_ELECTRONENERGY: Level 2 Energetic Ion Spectrometer Electron Spectra Srvy - B. Mauk (JHU/APL)
MMS3_EPD-EIS_SRVY_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Srvy - B. Mauk (JHU/APL)
MMS3_EPD-EIS_SRVY_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Srvy - B. Mauk (JHU/APL)
MMS3_FEEPS_BRST_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS3_FEEPS_BRST_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS3_FEEPS_SRVY_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS3_FEEPS_SRVY_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS3_FGM_BRST_L2: Level2 Flux Gate Magnetometer Burst DC Magnetic Field for MMS Satellite Number 3 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS3_FGM_SRVY_L2: Level2 Flux Gate Magnetometer Combined Fast/Slow Survey DC Magnetic Field for MMS Satellite Number 3 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS3_FPI_BRST_L2_DES-DIST: MMS Satellite Number 3 Dual Electron Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_BRST_L2_DES-MOMS: MMS Satellite Number 3 Dual Electron Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_BRST_L2_DES-PARTMOMS: MMS Satellite Number 3 Dual Electron Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_BRST_L2_DIS-DIST: MMS Satellite Number 3 Dual Ion Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_BRST_L2_DIS-MOMS: MMS Satellite Number 3 Dual Ion Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_BRST_L2_DIS-PARTMOMS: MMS Satellite Number 3 Dual Ion Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DES-DIST: MMS Satellite Number 3 Dual Electron Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DES-MOMS: MMS Satellite Number 3 Dual Electron Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DES-PARTMOMS: MMS Satellite Number 3 Dual Electron Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DIS-DIST: MMS Satellite Number 3 Dual Ion Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DIS-MOMS: MMS Satellite Number 3 Dual Ion Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_FPI_FAST_L2_DIS-PARTMOMS: MMS Satellite Number 3 Dual Ion Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS3_HPCA_BRST_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS3_HPCA_BRST_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS3_HPCA_SRVY_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS3_HPCA_SRVY_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS3_HPCA_SRVY_L2_TOF-COUNTS: Level 1b> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS3_MEC_BRST_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_MEC_BRST_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_MEC_BRST_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_MEC_SRVY_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_MEC_SRVY_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_MEC_SRVY_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 3 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS3_R0_SUMMARY: Links to MMS-3 pre-generated Quicklook Summary plots - James Burch (SWRI)
MMS3_SCM_BRST_L2_SCB: Level 2 Search Coil Magnetometer AC Magnetic Field Burst (8192S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS3_SCM_BRST_L2_SCHB: Level 2 Search Coil Magnetometer AC Magnetic Field High Burst (16384S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS3_SCM_SRVY_L2_SCSRVY: Level 2 Search Coil Magnetometer AC Magnetic Field Survey (32S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS4_ASPOC_SRVY_L2: Level 2 Active Spacecraft Potential Control Survey Data - K. Torkar, R. Nakamura (IWF)
MMS4_DSP_FAST_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS4_DSP_FAST_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS4_DSP_SLOW_L2_BPSD: search coil magnetometer spectral density - J. Burch, R. Ergun, O. Le Contel (SWRI, LASP, LPP)
MMS4_DSP_SLOW_L2_EPSD: electric spectral density - J. Burch, R. Ergun (SWRI, LASP)
MMS4_EDI_BRST_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS4_EDI_BRST_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS4_EDI_BRST_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS4_EDI_BRST_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS4_EDI_SRVY_L2_AMB: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS4_EDI_SRVY_L2_AMB-PM2: Level 2 EDI Ambient electron flux - Roy Torbert, Hans Vaith (UNH)
MMS4_EDI_SRVY_L2_EFIELD: Level 2 EDI electric field - Roy Torbert and Hans Vaith (UNH)
MMS4_EDI_SRVY_L2_Q0: Level 2 EDI Quality 0 Counts - Roy Torbert, Hans Vaith (UNH)
MMS4_EDP_BRST_L2_DCE: MMS4 L2 (brst), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_BRST_L2_HMFE: MMS4 l2 (brst), 3D HMFE Electric field - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS4_EDP_BRST_L2_SCPOT: MMS 4 dual probe scpot (brst), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_FAST_L2_DCE: MMS4 L2 (fast), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_FAST_L2_SCPOT: MMS 4 dual probe scpot (fast), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_SLOW_L2_DCE: MMS4 L2 (slow), 3D Electric field - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_SLOW_L2_SCPOT: MMS 4 dual probe scpot (slow), Spacecraft potential - J.Burch, R.Ergun, P.Lindqvist. (SWRI, LASP, KTH)
MMS4_EDP_SRVY_L2_HFESP: MMS4 L2 (srvy), HF ACE Spectra - Burch, J, Ergun, R., Lindqvist, P. (SwRI, LASP, KTH)
MMS4_EPD-EIS_BRST_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Brst - B. Mauk (JHU/APL)
MMS4_EPD-EIS_BRST_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Brst - B. Mauk (JHU/APL)
MMS4_EPD-EIS_SRVY_L2_ELECTRONENERGY: Level 2 Energetic Ion Spectrometer Electron Spectra Srvy - B. Mauk (JHU/APL)
MMS4_EPD-EIS_SRVY_L2_EXTOF: Level 2 Energetic Ion Spectrometer EnergyxTOF Srvy - B. Mauk (JHU/APL)
MMS4_EPD-EIS_SRVY_L2_PHXTOF: Level 2 Energetic Ion Spectrometer PulseHeightxTOF Srvy - B. Mauk (JHU/APL)
MMS4_FEEPS_BRST_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS4_FEEPS_BRST_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Burst Data - STP (LASP)
MMS4_FEEPS_SRVY_L2_ELECTRON: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS4_FEEPS_SRVY_L2_ION: Level 2 Flys Eye Energetic Particle Sensor Survey Data - STP (LASP)
MMS4_FGM_BRST_L2: Level2 Flux Gate Magnetometer Burst DC Magnetic Field for MMS Satellite Number 4 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS4_FGM_SRVY_L2: Level2 Flux Gate Magnetometer Combined Fast/Slow Survey DC Magnetic Field for MMS Satellite Number 4 - J. Burch, C. Russell, W. Magnus (SWRI, UCLA, IWF)
MMS4_FPI_BRST_L2_DES-DIST: MMS Satellite Number 4 Dual Electron Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_BRST_L2_DES-MOMS: MMS Satellite Number 4 Dual Electron Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_BRST_L2_DES-PARTMOMS: MMS Satellite Number 4 Dual Electron Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_BRST_L2_DIS-DIST: MMS Satellite Number 4 Dual Ion Spectrometer Burst-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_BRST_L2_DIS-MOMS: MMS Satellite Number 4 Dual Ion Spectrometer Burst-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_BRST_L2_DIS-PARTMOMS: MMS Satellite Number 4 Dual Ion Spectrometer Burst-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DES-DIST: MMS Satellite Number 4 Dual Electron Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DES-MOMS: MMS Satellite Number 4 Dual Electron Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DES-PARTMOMS: MMS Satellite Number 4 Dual Electron Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DIS-DIST: MMS Satellite Number 4 Dual Ion Spectrometer FastSurvey-resolution instrument distributions - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DIS-MOMS: MMS Satellite Number 4 Dual Ion Spectrometer FastSurvey-resolution distribution moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_FPI_FAST_L2_DIS-PARTMOMS: MMS Satellite Number 4 Dual Ion Spectrometer FastSurvey-resolution partial moments - J. Burch, B. Giles (SwRI, GSFC)
MMS4_HPCA_BRST_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS4_HPCA_BRST_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS4_HPCA_SRVY_L2_ION: Level 2> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS4_HPCA_SRVY_L2_MOMENTS: Level 2 Moments> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS4_HPCA_SRVY_L2_TOF-COUNTS: Level 1b> Hot Plasma Composition Analyzer - J. Burch, S. Fuselier (SWRI)
MMS4_MEC_BRST_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_MEC_BRST_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_MEC_BRST_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_MEC_SRVY_L2_EPHT89D: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_MEC_SRVY_L2_EPHT89Q: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_MEC_SRVY_L2_EPHTS04D: Magnetic ephemeris and support data for MMS satellite number 4 - M. G. Henderson, S. K. Morley (Los Alamos National Laboratory (LANL))
MMS4_R0_SUMMARY: Links to MMS-4 pre-generated Quicklook Summary plots - James Burch (SWRI)
MMS4_SCM_BRST_L2_SCB: Level 2 Search Coil Magnetometer AC Magnetic Field Burst (8192S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS4_SCM_BRST_L2_SCHB: Level 2 Search Coil Magnetometer AC Magnetic Field High Burst (16384S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MMS4_SCM_SRVY_L2_SCSRVY: Level 2 Search Coil Magnetometer AC Magnetic Field Survey (32S/s) Data - J. Burch, O. Le Contel (SWRI, LPP)
MSL_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
MSL_RAD_OBS-L1: MSL/RAD Level 1 observational counter data - D. Hassler (SwRI-Boulder)
MSL_RAD_OBS-L2: MSL/RAD Level 2 observational radiation data - D. Hassler (SwRI-Boulder)
MUNIN_M1_MDSE: MUNIN, MEDUSA IDFS format - David Winningham (Southwest Research Institute)
MUNIN_M1_MDSI: MUNIN, MEDUSA IDFS format - David Winningham (Southwest Research Institute)
MUNIN_M1_OA: MUNIN, Orbit and attitude data IDFS format - Rymd Plasma Gruppen (Swedish Institute of Space Physics)
MVN_INSITU_KP-4SEC: MAVEN In-situ Key Parameters - B.M. Jakosky (LASP/U. Colorado)
MVN_MAG_L2-SUNSTATE-1SEC: MAVEN Magnetometer Sun-State 1 Second Magnetic Field - J. Connerney (NASA GSFC)
MVN_SEP_L2_S1-CAL-SVY-FULL: DERIVED FROM: MAVEN SEP (Solar Energetic Particle) Instrument - D. Larson (davin@ssl.berkeley.edu) (U.C. Berkeley Space Sciences Laboratory)
MVN_SEP_L2_S2-CAL-SVY-FULL: DERIVED FROM: MAVEN SEP (Solar Energetic Particle) Instrument - D. Larson (davin@ssl.berkeley.edu) (U.C. Berkeley Space Sciences Laboratory)
MVN_STA_L2_D8-12R1E: MAVEN Supra-Thermal And Thermal Ion Composition Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
MVN_STA_L2_D9-12R64E: MAVEN Supra-Thermal And Thermal Ion Composition Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
MVN_STA_L2_DA-1R64E: MAVEN Supra-Thermal And Thermal Ion Composition Particle Distributions - J. P. McFadden (U.C. Berkeley Space Sciences Laboratory)
MVN_SWE_L2_ARC3D: DERIVED FROM: MAVEN SWEA (Solar Wind Electron Analyzer) 3D Distributions - David L. Mitchell (mitchell@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
MVN_SWE_L2_ARCPAD: DERIVED FROM: MAVEN SWEA (Solar Wind Electron Analyzer) Pitch Angle Distributions - David L. Mitchell (mitchell@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
MVN_SWE_L2_SVY3D: DERIVED FROM: MAVEN SWEA (Solar Wind Electron Analyzer) 3D Distributions - David L. Mitchell (mitchell@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
MVN_SWE_L2_SVYPAD: DERIVED FROM: MAVEN SWEA (Solar Wind Electron Analyzer) Pitch Angle Distributions - David L. Mitchell (mitchell@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
MVN_SWE_L2_SVYSPEC: DERIVED FROM: MAVEN SWEA (Solar Wind Electron Analyzer) Energy Spectra - David L. Mitchell (mitchell@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
MVN_SWI_L2_COARSEARC3D: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Coarse 3d Distributions - J.S. Halekas (U Iowa)
MVN_SWI_L2_COARSESVY3D: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Coarse 3d Distributions - J.S. Halekas (U Iowa)
MVN_SWI_L2_FINEARC3D: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Fine 3d Distributions - J.S. Halekas (U Iowa)
MVN_SWI_L2_FINESVY3D: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Fine 3d Distributions - J.S. Halekas (U Iowa)
MVN_SWI_L2_ONBOARDSVYMOM: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Onboard Moments - J.S. Halekas (U Iowa)
MVN_SWI_L2_ONBOARDSVYSPEC: DERIVED FROM: MAVEN SWIA (Solar Wind Ion Analyzer), Onboard Energy Spectra - J.S. Halekas (U Iowa)
NEPTUNE_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
NEPTUNE_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
NEW-HORIZONS_PEPSSI_COSMIC-RAY-CORRECTED-COUNT-RATE-CRCPS: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) corrected cosmic ray count per second - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_COSMIC-RAY-CORRECTED-COUNT-RATE-CRCPS-SPECTRA: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) corrected cosmic ray count per second - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_COSMIC-RAY-CORRECTED-FLUX-CRFLUX-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) background corrected cosmic ray flux in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_COSMIC-RAY-CORRECTED-FLUX-CRFLUX-SPECTRA-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) background corrected cosmic ray flux in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-COUNT-RATE-TOF-LCPS-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) 'Doubles' low energy events counts per second, time-of-flight (TOF) only, ~2-250 keV/nuc He+ in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-COUNT-RATE-TOF-LCPS-B: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) 'Doubles' low energy events counts per second, time-of-flight (TOF) only, ~2-250 keV/nuc He+ in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-COUNT-RATE-TOF-LCPS-SPECTRA-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) background corrected cosmic ray flux in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-COUNT-RATE-TOF-LCPS-SPECTRA-B: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) background corrected cosmic ray flux in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-DIFF-INTENSITY-TOF-LFLUX-A: PEPSSI>Pluto Energetic Particle Spectrometer Science Investigation suprathermal (lowest energy) particle time-of-flight (TOF) differential intensity in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-DIFF-INTENSITY-TOF-LFLUX-B: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) background corrected cosmic ray flux in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-DIFF-INTENSITY-TOF-LFLUX-SPECTRA-A: PEPSSI>Pluto Energetic Particle Spectrometer Science Investigation suprathermal (lowest energy) particle time-of-flight (TOF) differential intensity in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_DOUBLES-DIFF-INTENSITY-TOF-LFLUX-SPECTRA-B: PEPSSI>Pluto Energetic Particle Spectrometer Science Investigation suprathermal (lowest energy) particle time-of-flight (TOF) differential intensity in calibration regime 'A' or 'B' - Dr. Ralph L.McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-COUNT-RATE-BCPS-A: New Horizons NH Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-COUNT-RATE-BCPS-B: New Horizons NH Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-COUNT-RATE-BCPS-SPECTRA-A: New Horizons NH Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-COUNT-RATE-BCPS-SPECTRA-B: New Horizons NH Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-DIFF-INTENSITY-BFLUX-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-DIFF-INTENSITY-BFLUX-B: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-DIFF-INTENSITY-BFLUX-SPECTRA-A: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW-HORIZONS_PEPSSI_TRIPLES-DIFF-INTENSITY-BFLUX-SPECTRA-B: New Horizons Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) Box-shaped slab triples count per second, time of flight (TOF) vs energy space, ~15 keV to 1 MeV, H, He, O (CNO group) in calibration regime 'A' or 'B' - Dr. Ralph L. McNutt, Jr (Johns Hopkins University Applied Physics Laboratory)
NEW_HORIZONS_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
NEW_HORIZONS_SWAP_PICKUP-IONS: Data from New Horizons SWAP instrument - David J. McComas (Princeton)
NEW_HORIZONS_SWAP_PICKUP-IONS-HISTOGRAM: Data from New Horizons SWAP instrument - David J. McComas (Princeton)
NEW_HORIZONS_SWAP_SOLAR-WIND: Data from New Horizons SWAP instrument - David J. McComas (Princeton)
NOAA05_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA06_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA07_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA08_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA10_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA12_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA14_MEPED1MIN_SEM: 1 minute re-processed particle count rates, fluxes, and model fields, SEM MEPED, NOAA-05/TIROS-N/POES 5-14 Data Archive - Shing F. Fung (SPDF, GSFC/NASA)
NOAA15_POES-SEM2_FLUXES-2SEC: NOAA15 POES-SEM2 2-second Particle Precipitation Data [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
NOAA16_POES-SEM2_FLUXES-2SEC: NOAA16 POES-SEM2 2-second Particle Precipitation Data [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
NOAA18_POES-SEM2_FLUXES-2SEC: NOAA18 POES-SEM2 2-second Particle Precipitation Data [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
NOAA19_POES-SEM2_FLUXES-2SEC: NOAA19 POES-SEM2 2-second Particle Precipitation Data [Important: these data have known contamination problems: please consult Rob Redmon (sem.poes@noaa.gov) for usage recommendations.] - NGDC and SWPC (NOAA)
OMNI2_H0_MRG1HR: OMNI Combined, Definitive, Hourly IMF and Plasma Data, and Energetic Proton Fluxes, Time-Shifted to the Nose of the Earth's Bow Shock, plus Solar and Magnetic Indices - J.H. King, N. Papitashvili (ADNET, NASA GSFC)
OMNI_COHO1HR_MERGED_MAG_PLASMA: OMNI Combined merged hourly magnetic field, plasma and ephermis data - J.H. King, N. Papatashvilli (AdnetSystems, NASA GSFC)
OMNI_HRO2_1MIN: OMNI Combined, Definitive 1-minute IMF and Definitive Plasma Data Time-Shifted to the Nose of the Earth's Bow Shock, plus Magnetic Indices - J.H. King, N. Papatashvilli (AdnetSystems, NASA GSFC)
OMNI_HRO2_5MIN: OMNI Combined, Definitive 5-minute IMF and Definitive Plasma, and Energetic Proton Fluxes, Time-Shifted to the Nose of the Earth's Bow Shock, plus Magnetic Indices - J.H. King, N. Papatashvilli (AdnetSystems, NASA GSFC)
OMNI_HRO_1MIN: OMNI Combined, Definitive, 1-minute IMF and Plasma Data Time-Shifted to the Nose of the Earth's Bow Shock, plus Magnetic Indices - J.H. King, N. Papatashvilli (AdnetSystems, NASA GSFC)
OMNI_HRO_5MIN: OMNI Combined, Definitive, 5-minute IMF and Plasma, and Energetic Proton Fluxes, Time-Shifted to the Nose of the Earth's Bow Shock, plus Magnetic Indices - J.H. King, N. Papatashvilli (AdnetSystems, NASA GSFC)
PHOBOS2_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PHOBOS2_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PIONEER10_COHO1HR_MERGED_MAG_PLASMA: Pioneer-10 merged hourly magnetic field, plasma and ephermis data - E.J. Smith (HVM) and A. Barnes (PLS) (NASA JPL/AMES)
PIONEER10_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PIONEER10_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PIONEER10_MAG_1MIN_MAGNETIC_FIELD: 1 min averaged magnetic field - Edward Smith (JPL NASA)
PIONEER11_COHO1HR_MERGED_MAG_PLASMA: Pioner-11 merged hourly magnetic field, plasma and ephermis data - E.J. Smith (HVM) and A. Barnes (PLS) (NASA JPL/AMES)
PIONEER11_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PIONEER11_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PIONEER6_R0_MAGPLASMA: Pioneer6 merged magnetic field and plasma hourly data from COHOWeb Service
PIONEER7_R0_MAGPLASMA: Pioneer7 merged magnetic field and plasma hourly data from COHOWeb Service
PIONEERVENUS_COHO1HR_MERGED_MAG_PLASMA: PioneerVenus merged magnetic field and plasma hourly data from COHOWeb Service - Dr. T. C. Russell (magnetic field), Dr. Aaron Barnes (plasma) (UCLA, NASA/Ames)
PIONEERVENUS_MERGED_SOLAR-WIND_10M: Pioneer Venus Orbiter 10-minute merged solar wind data - Dr. C. T. Russell (magnetic field), Dr. Aaron Barnes (plasma) (UCLA, NASA/Ames)
PLUTO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PLUTO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PMC-TURBO_L1_BOLIDE_VBC: PMC-Turbo/BOLIDE Rayleigh lidar PMC data 20m 10s resolution - Bernd Kaifler, bernd.kaifler@dlr.de (DLR, IPA)
POLAR_HYDRA_MOMENTS-14SEC: Polar Fast Plasma Analyzer 13.8 second Resolution Moments - J. Scudder (U of Iowa)
PO_10MINATT_EFI: Polar Spacecraft Attitude in GSE Coordinates - Mozer (UC Berkeley)
PO_6SECEDSC_EFI: Polar Electric Field (x,y) in Despun Spacecraft Coordinates - Mozer (UC Berkeley)
PO_6SECPOTLDENS_EFI: Polar Spacecraft Potential and Inferred Plasma Density - Mozer (UC Berkeley)
PO_AT_DEF: Polar Definitive Attitude Data
PO_AT_PRE: Polar Predicted Attitude Data
PO_EJ_VIS: Polar Visible Imaging System, Earth Camera Images, processed - Louis A. Frank (The University of Iowa)
PO_H0_CAM: Ion Fluxes 1-200 keV/q @ 3-minute resolution, Polar CAMMICE - R. Friedel (Lanl)
PO_H0_HYD: Polar Fast Plasma Analyzer 13.8 second Resolution Parameters - J. Scudder (U of Iowa)
PO_H0_PWI: Polar Plasma Wave Instrument, MCA - D. Gurnett (U. Iowa)
PO_H0_TID: Polar TIDE H+,O+,He+ High Time Resolution Data (before 10/01/96) - Thomas E. Moore (Goddard Space Flight Center)
PO_H0_TIM: Polar Toroidal Imaging Mass-Angle Spectrograph, High Time Resolution data - W.K. Peterson (LASP/University of Colorado)
PO_H0_UVI: Polar Ultraviolet Imager, High Res. - G. Parks (U. Washington)
PO_H1_PWI: Polar Plasma Wave Instrument, Step Frequency Receivers A & B - D. Gurnett (U. Iowa)
PO_H1_TID: Polar TIDE Total Ion High Time Resolution Data (after 12/7/96) - Thomas E. Moore (Goddard Space Flight Center)
PO_H1_UVI: Polar Ultraviolet Imager, High Res. - G. Parks (U. Washington)
PO_H2_PWI: Polar Plasma Wave Instrument, Low Frequency Waveform Receiver, ~0.01 sec resolution fields - D. Gurnett (U. Iowa)
PO_H2_TIM: H+, O+, He+ and He++ upflowing fluxes, from Polar TIMAS - W.K. Peterson (LASP/University of Colorado)
PO_H3_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver, 16 kHz Time Domain Fields - D. Gurnett (U. Iowa)
PO_H4_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver, 2 kHz, Time Domain Fields - D. Gurnett (U. Iowa)
PO_H5_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver, 16 kHz, Time Domain Fields. - D. Gurnett (U. Iowa)
PO_H7_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver, 6-channel (~1.5 usec resolution) fields - D. Gurnett (U. Iowa)
PO_H8_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver - D. Gurnett (U. Iowa)
PO_H9_PWI: Polar Plasma Wave Instrument, High Frequency Waveform Receiver - D. Gurnett (U. Iowa)
PO_HYD_ENERGY_FLUX: Polar Fast Plasma Analyzer 13.8 second Resolution Moments - J. Scudder (U of Iowa)
PO_K0_CAM: CAMMICE Energetic particles & Ion composition, Key parameters - T. A. Fritz (Boston University)
PO_K0_CEP: CEPPAD Energetic particles & angular distribution, Key parameters - J. B.Blake (Aerospace Corp. )
PO_K0_EFI: Polar Electric Field Instrument, Key Parameters - F. Mozer (UC Berkeley)
PO_K0_GIFWALK: Links to Polar KP pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
PO_K0_HYD: Polar Fast Plasma Analyzer, Key Parameters - J. Scudder (U of Iowa)
PO_K0_MFE: Polar Magnetic Field,Key Parameters - C.T. Russell (UCLA)
PO_K0_PIX: Polar Ionospheric X-ray Imaging Experiment Key Parameters - D. Chenette (Lockheed)
PO_K0_PWI: Polar Plasma Wave Instrument, Key Parameters - D. Gurnett (U. Iowa)
PO_K0_SPHA: Polar Spin Phase Key Parameters
PO_K0_UVI: Polar Ultraviolet Imager, Key Parameters - G. Parks (U. Washington)
PO_K0_VIS: Polar Visible Imaging System Key Parameters - Louis A. Frank (The University of Iowa)
PO_K1_TIM: Polar Toroidal Imaging Mass-Angle Spectrograph, Supplemental Key Parameters - W.K. Peterson (LASP/University of Colorado)
PO_K1_VIS: Polar Visible Imaging System Earth Camera Key Parameter - Louis A. Frank (The University of Iowa)
PO_LEVEL1_UVI: Polar UVI Level-1 Full Resolution Imager Data - G. Parks (U. Washington)
PO_OR_DEF: Polar Definitive Orbit Data
PO_OR_PRE: Polar Predicted Orbit Data
PO_PA_DEF: Polar Platform Attitude Definitive data
PO_VIS_EARTH-CAMERA-CALIBRATED: Polar Visible Imaging System (VIS) Earth Camera Images at ~4 minute cadence - Louis A. Frank (The University of Iowa)
PO_VIS_VISIBLE-IMAGER-CALIBRATED: Polar Visible Imaging System (VIS) Low Res. Camera - Louis A. Frank (The University of Iowa)
PSP_COHO1HR_MERGED_MAG_PLASMA: Merged hourly magnetic field, plasma, proton fluxes, and ephermis data of PSP - Natalia Papitashvili (NASA/GSFC)
PSP_FLD_L2_AEB: PSP FIELDS AEB - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_BPF_DV12HG: PSP FIELDS Level 2 DFB AC Bandpass Filter dV12hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_BPF_DV34HG: PSP FIELDS Level 2 DFB AC Bandpass Filter dV34hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_BPF_SCMULFHG: PSP FIELDS Level 2 DFB AC Bandpass Filter SCMulfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_BPF_SCMUMFHG: PSP FIELDS Level 2 DFB AC Bandpass Filter SCMumfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_DV12HG: psp fld l2 dfb ac spec dV12hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_DV34HG: psp fld l2 dfb ac spec dV34hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMDLFHG: psp fld l2 dfb ac spec SCMdlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMELFHG: psp fld l2 dfb ac spec SCMelfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMFLFHG: psp fld l2 dfb ac spec SCMflfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMMF: psp fld l2 dfb ac spec SCMmf - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMULFLG: psp fld l2 dfb ac spec SCMulflg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_SCMVLFHG: psp fld l2 dfb ac spec SCMvlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_SPEC_V5HG: psp fld l2 dfb ac spec V5hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_XSPEC_DV12HG_DV34HG: PSP FLD L2 DFB AC XSPEC DV12HG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_XSPEC_SCMDLFHG_SCMELFHG: PSP FLD L2 DFB AC XSPEC SCMDLFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_XSPEC_SCMDLFHG_SCMFLFHG: PSP FLD L2 DFB AC XSPEC SCMDLFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_AC_XSPEC_SCMELFHG_SCMFLFHG: PSP FLD L2 DFB AC XSPEC SCMELFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DBM_DVAC: PSP FIELDS Level 2 DFB DBM Waveform Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DBM_DVDC: PSP FIELDS Level 2 DFB DBM Waveform Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DBM_SCM: PSP FIELDS Level 2 DFB DBM Waveform Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DBM_VAC: PSP FIELDS Level 2 DFB DBM Waveform Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DBM_VDC: PSP FIELDS Level 2 DFB DBM Waveform Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_BPF_DV12HG: PSP FIELDS Level 2 DFB DC Bandpass Filter dV12hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_BPF_DV34HG: PSP FIELDS Level 2 DFB DC Bandpass Filter dV34hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_BPF_SCMULFHG: PSP FIELDS Level 2 DFB DC Bandpass Filter SCMulfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_BPF_SCMVLFHG: PSP FIELDS Level 2 DFB DC Bandpass Filter SCMvlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_DV12HG: psp fld l2 dfb dc spec dV12hg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMDLFHG: psp fld l2 dfb dc spec SCMdlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMELFHG: psp fld l2 dfb dc spec SCMelfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMFLFHG: psp fld l2 dfb dc spec SCMflfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMULFHG: psp fld l2 dfb dc spec SCMulfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMVLFHG: psp fld l2 dfb dc spec SCMvlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_SPEC_SCMWLFHG: psp fld l2 dfb dc spec SCMwlfhg - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_XSPEC_SCMDLFHG_SCMELFHG: PSP FLD L2 DFB DC XSPEC SCMDLFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_XSPEC_SCMDLFHG_SCMFLFHG: PSP FLD L2 DFB DC XSPEC SCMDLFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_XSPEC_SCMELFHG_SCMFLFHG: PSP FLD L2 DFB DC XSPEC SCMELFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_DC_XSPEC_SCMVLFHG_SCMWLFHG: PSP FLD L2 DFB DC XSPEC SCMVLFHG - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_WF_DVDC: PSP FIELDS Level 2 DFB Differential Voltage Waveform - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_WF_SCM: PSP FIELDS Level 2 DFB Search Coil Magnetometer Waveform - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_DFB_WF_VDC: PSP FIELDS Level 2 DFB Single Ended Antenna Voltage Waveform - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_F2_100BPS: PSP FIELDS F2-100bps Summary Telemetry - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_MAG_RTN: PSP FIELDS 4 samples per cycle cadence Fluxgate Magnetometer (MAG) data in RTN coordinates - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_MAG_RTN_1MIN: PSP FIELDS 1 minute cadence Fluxgate Magnetometer (MAG) data in RTN coordinates - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_MAG_SC: PSP FIELDS 4 samples per cycle cadence Fluxgate Magnetometer (MAG) data in SC coordinates - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_MAG_SC_1MIN: PSP FIELDS 1 minute cadence Fluxgate Magnetometer (MAG) data in SC coordinates - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_MAG_VSO: PSP FIELDS full cadence Fluxgate Magnetometer (MAG) data in VSO coordinates - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_RFS_BURST: PSP FIELDS RFS BURST Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_RFS_HFR: PSP FIELDS RFS HFR Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_RFS_LFR: PSP FIELDS RFS LFR Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L2_TDS_WF: PSP FIELDS TDS Wave-Form Burst Science Telemetry - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_DUST: PSP FIELDS Level 3 dust impact detection data - Stuart D. Bale (bale@berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_MERGED_SCAM_WF: PSP FIELDS Level 3 Merged Magnetic Field Waveform - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_RFS_HFR: PSP FIELDS RFS HFR Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_RFS_LFR: PSP FIELDS RFS LFR Data - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_RFS_LFR_QTN: PSP FIELDS Level 3 Electron Density Data from Radio Frequency Spectrometer (RFS) Low Frequency Receiver (LFR) Quasi-Thermal Noise (QTN) Spectroscopy - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_FLD_L3_SQTN_RFS_V1V2: Parker Solar Probe FIELDS Level 3 Simplified Quasi-Thermal Noise data, using the Radio Frequency Spectrometer spectra when connected to V1V2 dipole antenna - Stuart D. Bale (bale@ssl.berkeley.edu) (UC Berkeley Space Sciences Laboratory)
PSP_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PSP_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
PSP_ISOIS-EPIHI_L2-HET-RATES10: Parker Solar Probe ISOIS EPI-Hi Level 2 HET 10-second Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-HET-RATES300: Parker Solar Probe ISOIS EPI-Hi Level 2 HET 5-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-HET-RATES3600: Parker Solar Probe ISOIS EPI-Hi Level 2 HET Hourly Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-HET-RATES60: Parker Solar Probe ISOIS EPI-Hi Level 2 HET 1-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET1-RATES10: Parker Solar Probe ISOIS EPI-Hi Level 2 LET1 10-second Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET1-RATES300: Parker Solar Probe ISOIS EPI-Hi Level 2 LET1 5-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET1-RATES3600: Parker Solar Probe ISOIS EPI-Hi Level 2 LET1 Hourly Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET1-RATES60: Parker Solar Probe ISOIS EPI-Hi Level 2 LET1 1-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET2-RATES10: Parker Solar Probe ISOIS EPI-Hi Level 2 LET2 10-second Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET2-RATES300: Parker Solar Probe ISOIS EPI-Hi Level 2 LET2 5-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET2-RATES3600: Parker Solar Probe ISOIS EPI-Hi Level 2 LET2 Hourly Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-LET2-RATES60: Parker Solar Probe ISOIS EPI-Hi Level 2 LET2 1-minute Rates - David McComas (Princeton University)
PSP_ISOIS-EPIHI_L2-SECOND-RATES: Parker Solar Probe ISOIS EPI-Hi Level 2 one-second Rates - David McComas (Princeton University)
PSP_ISOIS-EPILO_L2-IC: Parker Solar Probe ISOIS EPI-Lo Level 2 Ion Composition - David McComas (Princeton University)
PSP_ISOIS-EPILO_L2-PE: Parker Solar Probe ISOIS EPI-Lo Level 2 Particle Energy - David McComas (Princeton University)
PSP_ISOIS_L2-EPHEM: Parker Solar Probe ISOIS Level 2 ephem - David McComas (Princeton University)
PSP_ISOIS_L2-SUMMARY: Parker Solar Probe ISOIS level 2 summary - David McComas (Princeton University)
PSP_SWP_SPA_SF0_L2_16AX8DX32E: Electron Differential Energy Flux at each measured energy/deflector step and anode of the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPA_SF0_L3_PAD: Electron Pitch Angle Distribution for the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPA_SF1_L2_32E: Electron Differential Energy Flux at each measured energy step, and averaged over all deflection steps and anodes of the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPB_SF0_L2_16AX8DX32E: Electron Differential Energy Flux at each measured energy/deflector step and anode of the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPB_SF0_L3_PAD: Electron Pitch Angle Distribution for the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPB_SF1_L2_32E: Electron Differential Energy Flux at each measured energy step, and averaged over all deflection steps and anodes of the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPC_L2I: L2 charge flux distributions - Justin C. Kasper (University of Michigan)
PSP_SWP_SPC_L3I: Parker Solar Probe/SWEAP/SPC level 3 ion data - Justin C. Kasper (University of Michigan)
PSP_SWP_SPE_SF0_L3_PAD: Electron Pitch Angle Distribution for the SPAN-Electron instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF00_L2_8DX32EX8A: Proton Differential Energy Flux at each measured energy/deflector step and anode of the SPAN-Ion instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF00_L3_MOM: Partial moments of the Proton distribution function in the SPAN-Ion instrument, PSP spacecraft, and RTN coordinate systems. User should be aware that the full ion distribution is typically NOT in the FOV of the instrument. - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF00_L3_MOM_INST: Partial moments of the Proton distribution function in the instrument frame of reference. User should be aware that the full ion distribution is typically NOT in the FOV of the instrument. - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF01_L2_8DX32EX8A: Proton-contaminated Alpha Differential Energy Flux at each measured energy/deflector step and anode of the SPAN-Ion instrument - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF0A_L3_MOM: Partial moments of the Alpha distribution function in the SPAN-Ion instrument, PSP spacecraft, and RTN coordinate systems. User should be aware that the full ion distribution is typically NOT in the FOV of the instrument. - J. Kasper (Univ. of Michigan)
PSP_SWP_SPI_SF0A_L3_MOM_INST: Partial moments of the Alpha distribution function in the instrument frame of reference. User should be aware that the full ion distribution is typically NOT in the FOV of the instrument. - J. Kasper (Univ. of Michigan)
RBSP-A-RBSPICE_LEV-2_ESRHELT: RBSP_H0_RBSPICE_ESR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_ESRLEHT: RBSP_H0_RBSPICE_ESR_LEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_ISRHELT: RBSP_H0_RBSPICE_ISR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_TOFXEH: RBSP_H0_RBSPICE_TOFxE_H - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_TOFXEION: RBSP_H0_RBSPICE_TOFxE_Ion - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_TOFXENONH: RBSP_H0_RBSPICE_TOFxE_nonH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_TOFXPHHHELT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-2_TOFXPHHLEHT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_ESRHELT: rbsp-a-rbspice_level_3_esrhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_ESRLEHT: rbsp-a-rbspice_level_3_esrleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEH: rbsp-a-rbspice_level_3_tofxeh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEHE: rbsp-a-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEHE-0: rbsp-a-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEION: rbsp-a-rbspice_level_3_tofxeion - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEO: rbsp-a-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXEO-0: rbsp-a-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHHHELT: rbsp-a-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHHLEHT: rbsp-a-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHOHELT: rbsp-a-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHOLEHT: rbsp-a-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_ESRHELT: rbsp-a-rbspice_level_3_ESRHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_ESRLEHT: rbsp-a-rbspice_level_3_ESRLEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_ISRHELT: rbsp-a-rbspice_level_3_ISRHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_TOFXEH: rbsp-a-rbspice_level_3_TOFXEH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_TOFXEION: rbsp-a-rbspice_level_3_TOFXEION - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_TOFXENONH: rbsp-a-rbspice_level_3_TOFXENONH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_TOFXPHHHELT: rbsp-a-rbspice_level_3_TOFXPHHHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A-RBSPICE_LEV-3_TOFXPHHLEHT: rbsp-a-rbspice_level_3_TOFXPHHLEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-A_DENSITY_EMFISIS-L4: Density and other parameters inferred by digitizing the trace on the spectrograms. - Craig Kletzing (University of Iowa)
RBSP-A_HFR-SPECTRA-BURST_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-A_HFR-SPECTRA-MERGED_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-A_HFR-SPECTRA_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-A_HFR-WAVEFORM_EMFISIS-L2: High Frequency Receiver Waveform - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_1SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_1SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_1SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_1SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_1SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_4SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_4SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_4SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_4SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_4SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_HIRES-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_HIRES-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_HIRES-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_HIRES-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_HIRES-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_MAGNETOMETER_UVW_EMFISIS-L2: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-A_WFR-SPECTRAL-MATRIX-DIAGONAL-MERGED_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-A_WFR-SPECTRAL-MATRIX-DIAGONAL_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-A_WFR-SPECTRAL-MATRIX_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-A_WFR-WAVEFORM-CONTINUOUS-BURST_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-A_WFR-WAVEFORM_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-A_WNA-SURVEY-SHEATH-CORRECTED-E_EMFISIS-L4: Probes-A EMFISIS wave normal angle products and sheath corrected electric field level Level-4 - Craig Kletzing (University of Iowa)
RBSP-A_WNA-SURVEY_EMFISIS-L4: Probes-A EMFISIS wave normal angle products level Level-4 - Craig Kletzing (University of Iowa)
RBSP-B-RBSPICE_LEV-2_ESRHELT: RBSP_H0_RBSPICE_ESR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_ESRLEHT: RBSP_H0_RBSPICE_ESR_LEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_ISRHELT: RBSP_H0_RBSPICE_ISR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_TOFXEH: RBSP_H0_RBSPICE_TOFxE_H - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_TOFXEION: RBSP_H0_RBSPICE_TOFxE_Ion - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_TOFXENONH: RBSP_H0_RBSPICE_TOFxE_nonH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_TOFXPHHHELT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-2_TOFXPHHLEHT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_ESRHELT: rbsp-b-rbspice_level_3_esrhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_ESRLEHT: rbsp-b-rbspice_level_3_esrleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEH: rbsp-b-rbspice_level_3_tofxeh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE-0: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEION: rbsp-b-rbspice_level_3_tofxeion - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO-0: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHHELT: rbsp-b-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHLEHT: rbsp-b-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOHELT: rbsp-b-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOLEHT: rbsp-b-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_ESRHELT: rbsp-b-rbspice_level_3_ESRHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_ESRLEHT: rbsp-b-rbspice_level_3_ESRLEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_ISRHELT: rbsp-b-rbspice_level_3_ISRHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_TOFXEH: rbsp-b-rbspice_level_3_TOFXEH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_TOFXEION: rbsp-b-rbspice_level_3_TOFXEION - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_TOFXENONH: rbsp-b-rbspice_level_3_TOFXENONH - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_TOFXPHHHELT: rbsp-b-rbspice_level_3_TOFXPHHHELT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B-RBSPICE_LEV-3_TOFXPHHLEHT: rbsp-b-rbspice_level_3_TOFXPHHLEHT - Lou Lanzerotti (New Jersey Institute of Technology)
RBSP-B_DENSITY_EMFISIS-L4: Density and other parameters inferred by digitizing the trace on the spectrograms. - Craig Kletzing (University of Iowa)
RBSP-B_HFR-SPECTRA-BURST_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-B_HFR-SPECTRA-MERGED_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-B_HFR-SPECTRA_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)
RBSP-B_HFR-WAVEFORM_EMFISIS-L2: High Frequency Receiver Waveform - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_1SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_1SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_1SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_1SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_1SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_4SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_4SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_4SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_4SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_4SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_HIRES-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_HIRES-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_HIRES-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_HIRES-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_HIRES-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_MAGNETOMETER_UVW_EMFISIS-L2: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)
RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL-MERGED_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-B_WFR-SPECTRAL-MATRIX_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-B_WFR-WAVEFORM-CONTINUOUS-BURST_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-B_WFR-WAVEFORM_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)
RBSP-B_WNA-SURVEY-SHEATH-CORRECTED-E_EMFISIS-L4: Probes-B EMFISIS wave normal angle products and sheath corrected electric field Level-4 - Craig Kletzing (University of Iowa)
RBSP-B_WNA-SURVEY_EMFISIS-L4: Probes-B EMFISIS wave normal angle products level Level-4 - Craig Kletzing (University of Iowa)
RBSPA_EFW-L2_E-HIRES-UVW: DERIVED FROM: Reference for Spin Axis Vector in GSE - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L2_E-SPINFIT-MGSE: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L2_ESVY_DESPUN: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L2_FBK: Filterbank data product from RBSP-EFW - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L2_SPEC: Spectral data product from RBSP-EFW - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L2_VSVY-HIRES: Single-ended potential values for boom 1-6 - J. R. Wygant (University of Minnesota)
RBSPA_EFW-L3: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPA_EFW_BURST-WAVEFORM-UVW-L1: Burst Mode 1 (512 samples/sec) Electric and Magnetic Fields - J. R. Wygant
RBSPA_L2-1MIN_PSBR-RPS: Van Allen Probes/RPS Level 2 1-Minute Data - J. Mazur (The Aerospace Corporation)
RBSPA_L2_PSBR-RPS: Van Allen Probes/RPS Level 2 Data - J. Mazur (The Aerospace Corporation)
RBSPA_REL03_ECT-MAGEIS-L2: rbsp-a_ect-mageis-l2_pre - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)
RBSPA_REL03_ECT-REPT-SCI-L2: rbspa>Level 2 data for the REPT instrument - D. Baker (University of Colorado at Boulder)
RBSPA_REL03_ECT-REPT-SCI-L3: RBSP/ECT REPT Pitch Angle Resolved Electron and Proton Fluxes. Electron energies: 1.8 - 20 MeV. Proton energies: 21.25 - 4.74961e-316 MeV - D. Baker (University of Colorado at Boulder)
RBSPA_REL04_ECT-HOPE-MOM-L3: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPA_REL04_ECT-HOPE-PA-L3: Pitch angle resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPA_REL04_ECT-HOPE-SCI-L2: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPA_REL04_ECT-HOPE-SCI-L2SA: Spin averaged HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPA_REL04_ECT-MAGEIS-L3: 14 - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)
RBSPB_EFW-L2_E-HIRES-UVW: DERIVED FROM: Reference for Spin Axis Vector in GSE - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L2_E-SPINFIT-MGSE: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L2_ESVY_DESPUN: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L2_FBK: Filterbank data product from RBSP-EFW - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L2_SPEC: Spectral data product from RBSP-EFW - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L2_VSVY-HIRES: Single-ended potential values for boom 1-6 - J. R. Wygant (University of Minnesota)
RBSPB_EFW-L3: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)
RBSPB_EFW_BURST-WAVEFORM-UVW-L1: Burst Mode 1 (512 samples/sec) Electric and Magnetic Fields - J. R. Wygant
RBSPB_L2-1MIN_PSBR-RPS: Van Allen Probes/RPS Level 2 1-Minute Data - J. Mazur (The Aerospace Corporation)
RBSPB_L2_PSBR-RPS: Van Allen Probes/RPS Level 2 Data - J. Mazur (The Aerospace Corporation)
RBSPB_REL03_ECT-MAGEIS-L2: rbsp-a_ect-mageis-l2_pre - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)
RBSPB_REL03_ECT-REPT-SCI-L2: rbspb>Level 2 data for the REPT instrument - D. Baker (University of Colorado at Boulder)
RBSPB_REL03_ECT-REPT-SCI-L3: RBSP/ECT REPT Pitch Angle Resolved Electron and Proton Fluxes. Electron energies: 1.8 - 20 MeV. Proton energies: 21.25 - 4.94066e-324 MeV - D. Baker (University of Colorado at Boulder)
RBSPB_REL04_ECT-HOPE-MOM-L3: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPB_REL04_ECT-HOPE-PA-L3: Pitch angle resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPB_REL04_ECT-HOPE-SCI-L2: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPB_REL04_ECT-HOPE-SCI-L2SA: Spin averaged HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)
RBSPB_REL04_ECT-MAGEIS-L3: 16 - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)
RBSP_ECT-REPT-SCI-L3-SELESNICK-MODEL: RBSP/ECT REPT Monthly Intensities as a function of Energy, Pitch Angle and L-shell from the Selesnick model - D. Baker (University of Colorado at Boulder)
REACH-VID-101_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 101 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-102_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 102 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-105_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 105 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-108_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 108 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-113_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 113 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-114_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 114 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-115_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 115 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-116_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 116 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-133_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 133 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-134_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 134 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-135_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 135 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-136_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 136 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-137_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 137 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-138_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 138 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-139_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 139 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-140_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 140 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-148_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 148 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-149_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 149 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-162_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 162 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-163_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 163 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-164_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 164 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-165_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 165 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-166_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 166 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-169_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 169 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-170_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 170 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-171_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 171 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-172_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 172 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-173_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 173 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-175_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 175 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-176_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 176 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-180_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 180 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
REACH-VID-181_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 181 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)
RENU2_H0_EFIELD: H0 - RENU2 COWBOY Electric Field. - Marc Lessard, David Hysell (University of New Hampshire, Cornell University)
RENU2_H0_EPLAS: H0 - RENU2 EPLAS Electron Flux. - Marc Lessard (University of New Hampshire)
RENU2_H0_ERPAMAIN: H0 - RENU2 ERPA Thermal Electrons. - Marc Lessard (University of New Hampshire)
RENU2_H0_ERPASUB: H0 - RENU2 ERPA Thermal Electrons. - Marc Lessard (University of New Hampshire)
RENU2_H0_FGM: H0 - RENU2 Magnetic Field. - Marc Lessard (University of New Hampshire, Cornell University)
RENU2_H0_IG2: H0 - RENU2 ionization gauge - James Clemmons (University of New Hampshire)
RENU2_H0_PMT: H0 - RENU2 PMT Rayleighs. - Jim Hecht (University of New HampshireAerospace Corporation)
RENU2_H0_UVPMT: H0 - RENU2 UV PMT Counts. - Marc Lessard (University of New Hampshire)
RENU2_H0_VLF: H0 - RENU2 COWBOY Electric Field. - Marc Lessard, David Hysell (University of New Hampshire, Cornell University)
ROSETTA_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
ROSETTA_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
RS_K0_IPEI: ROCSAT-1(FORMOSAT-1)/IPEI, Key Parameters - Shin-Yi Su (Institution of Space Science, National Central University, Taiwan, R.O.C.)
SAKIGAKE_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SAKIGAKE_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SATURN_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SATURN_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SE_K0_AIS: SESAME Advanced Ionospheric Sounder, Key Parameters - J. Dudeney (British Antarctic Survey)
SE_K0_FPI: SESAME Fabry-Perot Interferometer, Key Parameters - J.R. Dudeney (British Antarctic Survey)
SE_K0_MAG: SESAME Fluxgate Magnetometer Key Parameters - J. Dudeney (British Antarctic Survey)
SE_K0_RIO: SESAME 30MHz Riometer Array, Key Parameters - J. Dudeney (British Antarctic Survey)
SE_K0_VLF: SESAME VLF/ELF Logger Experiment (VELOX)Key Parameters - J. Dudeney (British Antarctic Survey)
SNOE_L3_GEO: NO density, 100 - 150 km, geographic coordinates - Charles A. Barth (LASP/CU)
SNOE_L3_MAG: NO density, 100 - 150 km, geomagnetic coordinates - Charles A. Barth (LASP/CU)
SOHO_CELIAS-PM_30S: SOHO CELIAS-PM 30 second data - Robert Wimmer-Schweingruber (wimmer@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_CELIAS-PM_5MIN: SOHO CELIAS-PM 5 minute data - Robert Wimmer-Schweingruber (wimmer@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_CELIAS-SEM_15S: SOHO CELIAS-SEM 15 second data - Robert Wimmer-Schweingruber (wimmer@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_CELIAS-SEM_1DAY: SOHO CELIAS-SEM 1 day data - Robert Wimmer-Schweingruber (wimmer@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-10MIN: SOHO COSTEP-EPHIN Level3 intensity 10 minute data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-1DAY: SOHO COSTEP-EPHIN Level3 intensity 1 day data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-1HR: SOHO COSTEP-EPHIN Level3 intensity 1 hour data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-1MIN: SOHO COSTEP-EPHIN Level3 intensity 1 minute data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-30MIN: SOHO COSTEP-EPHIN Level3 intensity 30 minute data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_COSTEP-EPHIN_L3I-5MIN: SOHO COSTEP-EPHIN Level3 intensity 5 minute data - Bernd Heber (heber@physik.uni-kiel.de) (Christian Albrechts Universitat)
SOHO_ERNE-HED_L2-1MIN: SOHO ERNE-HED Level2 1 minute data - Rami Vainio (rami.vainio@utu.fi) (Space Research Laboratory)
SOHO_ERNE-LED_L2-1MIN: SOHO ERNE-LED Level2 1 minute data - Rami Vainio (rami.vainio@utu.fi) (Space Research Laboratory)
SOHO_ERNE_HEAVY-ION-1HR: SOHO ERNE heavy ion 1 hour data - Rami Vainio (rami.vainio@utu.fi) (Space Research Laboratory)
SOHO_ERNE_HEAVY-ION-5MIN: SOHO ERNE heavy ion 5 minute data - Rami Vainio (rami.vainio@utu.fi) (Space Research Laboratory)
SOHO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SOHO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SOLO_COHO1HR_MERGED_MAG_PLASMA: Merged hourly magnetic field, plasma, proton fluxes, and ephermis data of Solar Orbiter - Natalia Papitashvili (NASA/GSFC)
SOLO_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SOLO_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SOLO_L2_EPD-EPT-ASUN-BURST-ELE-CLOSE: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Anti-Sun direction, Burst, Electrons, Close mode - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-ASUN-BURST-ION: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Anti-Sun direction, Burst, Ions - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-ASUN-HCAD: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Anti-Sun direction, High Cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-ASUN-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Anti-Sun direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-NORTH-BURST-ELE-CLOSE: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, North direction, Burst, Electrons, Close mode - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-NORTH-BURST-ION: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, North direction, Burst, Ions - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-NORTH-HCAD: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, North direction, High Cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-NORTH-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, North direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SOUTH-BURST-ELE-CLOSE: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, South direction, Burst, Electrons, Close mode - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SOUTH-BURST-ION: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, South direction, Burst, Ions - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SOUTH-HCAD: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, South direction, High Cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SOUTH-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, South direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SUN-BURST-ELE-CLOSE: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Sun direction, Burst, Electrons, Close mode - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SUN-BURST-ION: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Sun direction, Burst, Ions - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SUN-HCAD: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Sun direction, High Cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-EPT-SUN-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Electron Proton Telescope, Sun direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-ASUN-BURST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, Anti-Sun direction, Burst - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-ASUN-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, Anti-Sun direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-NORTH-BURST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, North direction, Burst - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-NORTH-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, North direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-SOUTH-BURST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, South direction, Burst - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-SOUTH-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, South direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-SUN-BURST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, Sun direction, Burst - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-HET-SUN-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, High Energy Telescope, Sun direction, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-A-HEHIST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, A Telescope, Helium histogram - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-A-RATES-FAST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, A Telescope, Particle rates, fast cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-A-RATES-MEDIUM: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, A Telescope, Particle rates, medium cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-A-RATES-SLOW: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, A Telescope, Particle rates, slow cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-B-HEHIST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, B Telescope, Helium histogram - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-B-RATES-FAST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, B Telescope, Particle rates, fast cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-B-RATES-MEDIUM: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, B Telescope, Particle rates, medium cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-SIS-B-RATES-SLOW: Solar Orbiter, Level 2 Data, Energetic Particle Detector, Suprathermal Ion Spectrograph, B Telescope, Particle rates, slow cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-STEP-BURST: Solar Orbiter, Level 2 Data, Energetic Particle Detector, SupraThermal Electrons and Protons, Burst - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-STEP-HCAD: Solar Orbiter, Level 2 Data, Energetic Particle Detector, SupraThermal Electrons and Protons, High Cadence - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-STEP-MAIN: Solar Orbiter, Level 2 Data, Energetic Particle Detector, SupraThermal Electrons and Protons, Main product - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_EPD-STEP-RATES: Solar Orbiter, Level 2 Data, Energetic Particle Detector, SupraThermal Electrons and Protons, Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L2_MAG-RTN-BURST: Solar Orbiter Magnetometer Level 2 Burst Mode Data in RTN coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-RTN-LL: Solar Orbiter Magnetometer L2 Data derived from LL data - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-RTN-LL-1-MINUTE: Solar Orbiter Magnetometer L2 Data derived from LL data - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-RTN-NORMAL: Solar Orbiter Magnetometer Level 2 Normal Mode Data in RTN coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-RTN-NORMAL-1-MINUTE: Solar Orbiter Magnetometer Level 2 Normal Mode Data in RTN coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-SRF-BURST: Solar Orbiter Magnetometer Level 2 Burst Mode Data in SRF coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-SRF-LL: Solar Orbiter Magnetometer L2 Data derived from LL data - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-SRF-NORMAL: Solar Orbiter Magnetometer Level 2 Normal Mode Data in SRF coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-VSO-BURST: Solar Orbiter Magnetometer Level 2 Burst Mode Data in VSO coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-VSO-NORMAL: Solar Orbiter Magnetometer Level 2 Normal Mode Data in VSO coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_MAG-VSO-NORMAL-1-MINUTE: Solar Orbiter Magnetometer Level 2 Normal Mode Data in VSO coordinates - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_L2_RPW-HFR-SURV: Solar Orbiter Radio/Plasma Wave, HFR L2 parameters - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L2_RPW-LFR-SURV-ASM: Solar Orbiter, Level L2, Radio and Plasma Waves, Low Frequency Receiver, Averaged spectral matrices in survey mode (calibrated) - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L2_RPW-LFR-SURV-BP1: Solar Orbiter, Level L2, Radio and Plasma Waves, Low Frequency Receiver, Basic Parameters set 1 in survey mode (calibrated) - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L2_RPW-LFR-SURV-BP2: Solar Orbiter, Level L2, Radio and Plasma Waves, Low Frequency Receiver, Basic Parameters set 2 in survey mode (calibrated) - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L2_RPW-LFR-SURV-CWF-B: Solar Orbiter, Level 2, Radio and Plasma Waves, Low Frequency Receiver, Continous Waveform of magnetic data in survey mode - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L2_RPW-LFR-SURV-CWF-E: Solar Orbiter Radio/Plasma Wave, LFR L2 electric parameters - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L2_RPW-TDS-SURV-HIST1D: Solar Orbiter Radio/Plasma Wave, TDS L2 parameters - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L2_RPW-TDS-SURV-HIST2D: Solar Orbiter Radio/Plasma Wave, TDS L2 parameters - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L2_RPW-TDS-SURV-STAT: Solar Orbiter Radio/Plasma Wave, TDS L2R parameters - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L2_SWA-EAS-PAD-DEF: Solar Orbiter, Level L2, Solar Wind Analyser, Electron Analyser System, Pitch Angle Distributions, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS-PAD-DNF: Solar Orbiter, Level L2, Solar Wind Analyser, Electron Analyser System, Pitch Angle Distributions, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS-PAD-PSD: Solar Orbiter, Level L2, Solar Wind Analyser, Electron Analyser System, Pitch Angle Distributions, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-EFLUX: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-HIRES3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, High Resolution Nominal Mode 3D, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-HIRES3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, High Resolution Nominal Mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-HIRES3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, High Resolution Nominal Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-NM3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Nominal Mode 3D, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-NM3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Nominal Mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-NM3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Nominal Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-SS-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Single Energy Strahl, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-SS-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Single Energy Strahl, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-SS-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Single Energy Strahl, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-TM3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Trigger Mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-TM3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Trigger Mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS1-TM3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 1, Trigger Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-EFLUX: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-HIRES3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, High Resolution Nominal Mode 3D, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-HIRES3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, High Resolution Nominal mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-HIRES3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, High Resolution Nominal Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-NM3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Nominal Mode 3D, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-NM3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-NM3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Nominal Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-SS-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Single Energy Strahl, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-SS-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Single Energy Strahl, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-SS-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Single Energy Strahl, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-TM3D-DEF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Trigger Mode 3D, Differential Energy Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-TM3D-DNF: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Trigger Mode 3D, Differential Number Flux - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-EAS2-TM3D-PSD: Solar Orbiter, Level L2, Solar Wind Analyzer, Electron Analyser System 2, Trigger Mode 3D, Phase Space Density - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L2_SWA-HIS-HK: Solar Orbiter Level 2 Solar Wind Analyser Heavy Ion Sensor Housekeeping Parameters - S. Livi (SWRI)
SOLO_L2_SWA-HIS-PHA: Solar Orbiter Level 2 Solar Wind Analyser Heavy Ion Sensor Pulse Height Analyzed - S. Livi (SWRI)
SOLO_L2_SWA-HIS-RATES: Solar Orbiter Level 2 Solar Wind Analyser Heavy Ion Sensor Rates - S. Livi (SWRI)
SOLO_L2_SWA-PAS-EFLUX: Solar Orbiter Proton Analyser Sensor L2 data - OWEN Chris (MSSL-UCL, university College London - UK)
SOLO_L2_SWA-PAS-GRND-MOM: Solar Orbiter Proton Analyser Sensor L2 data - OWEN Chris (MSSL-UCL, university College London - UK)
SOLO_L2_SWA-PAS-VDF: Solar Orbiter Proton Analyser Sensor L2 data - OWEN Chris (MSSL-UCL, university College London - UK)
SOLO_L3_EPD-EPT-1DAY: Solar Orbiter, Level 3 Data, Energetic Particle Detector, Electron Proton Telescope, 1 day resolution data - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L3_EPD-EPT-1HOUR: Solar Orbiter, Level 3 Data, Energetic Particle Detector, Electron Proton Telescope, 1 hour resolution data - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L3_EPD-EPT-1MIN: Solar Orbiter, Level 3 Data, Energetic Particle Detector, Electron Proton Telescope, 1 minute resolution data - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_L3_MULTI-MAG-RPW-SCM-MERGED-RTN-256: Solar Orbiter, Level 3, MAG and RPW, Merged magnetic data sampled at 256 Hz - M. Kretzschmar ; T. Horbury ; M. Maksimovic (LPC2E, CNRS/Université d’Orléans/CNES ; Blackett Laboratory, Imperial College London ; LIRA, Observatoire de Paris/CNRS)
SOLO_L3_MULTI-MAG-RPW-SCM-MERGED-RTN-4096: Solar Orbiter, Level 3, MAG and RPW, Merged magnetic data sampled at 4096 Hz - M. Kretzschmar ; T. Horbury ; M. Maksimovic (LPC2E, CNRS/Université d’Orléans/CNES ; Blackett Laboratory, Imperial College London ; LIRA, Observatoire de Paris/CNRS)
SOLO_L3_MULTI-MAG-RPW-SCM-MERGED-SRF-256: Solar Orbiter, Level 3, MAG and RPW, Merged magnetic data sampled at 256 Hz - M. Kretzschmar ; T. Horbury ; M. Maksimovic (LPC2E, CNRS/Université d’Orléans/CNES ; Blackett Laboratory, Imperial College London ; LIRA, Observatoire de Paris/CNRS)
SOLO_L3_MULTI-MAG-RPW-SCM-MERGED-SRF-4096: Solar Orbiter, Level 3, MAG and RPW, Merged magnetic data sampled at 4096 Hz - M. Kretzschmar ; T. Horbury ; M. Maksimovic (LPC2E, CNRS/Université d’Orléans/CNES ; Blackett Laboratory, Imperial College London ; LIRA, Observatoire de Paris/CNRS)
SOLO_L3_RPW-BIA-DENSITY: Solar Orbiter Radio/Plasma Wave, LFR L3 plasma density derived from the spacecraft potential - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L3_RPW-BIA-DENSITY-10-SECONDS: Solar Orbiter Radio/Plasma Wave, LFR L3 plasma density derived from the spacecraft potential, downsampled - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L3_RPW-BIA-EFIELD: Solar Orbiter Radio/Plasma Wave, LFR L3 electric field vector - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L3_RPW-BIA-EFIELD-10-SECONDS: Solar Orbiter Radio/Plasma Wave, LFR L3 electric field vector, downsampled - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L3_RPW-BIA-SCPOT: Solar Orbiter Radio/Plasma Wave, LFR L3 spacecraft potential - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L3_RPW-BIA-SCPOT-10-SECONDS: Solar Orbiter Radio/Plasma Wave, LFR L3 spacecraft potential, downsampled - M.Maksimovic (CNRS, LIRA Observatoire de Paris-PSL)
SOLO_L3_RPW-BIA-VHT: Solar Orbiter Radio/Plasma Wave, LFR L3 de Hoffmann-Teller solar wind velocity - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L3_RPW-TNR-FP: Solar Orbiter Radio/Plasma Wave, data from plasma peak tracking L3 - M.Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_L3_SWA-EAS-NMPAD-PSD: Solar Orbiter, Level L3, Solar Wind Analyser, Electron Analyser System, Nominal mode pitch angle distributions in PSD units - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_L3_SWA-HIS-COMP-10MIN: Solar Orbiter, Level 3 Data, Solar Wind Analyser, Heavy Ion Sensor Composition 10 Minute Resolution - S. Livi (SWRI)
SOLO_LL02_EPD-EPT-ASUN-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Electron Proton Telescope, asun direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-EPT-NORTH-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Electron Proton Telescope, north direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-EPT-SOUTH-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Electron Proton Telescope, south direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-EPT-SUN-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Electron Proton Telescope, sun direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-HET-ASUN-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, High Energy Telescope, asun direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-HET-NORTH-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, High Energy Telescope, north direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-HET-SOUTH-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, High Energy Telescope, south direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-HET-SUN-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, High Energy Telescope, sun direction, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-SIS-A-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Suprathermal Ion Spectrograph A Telescope, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-SIS-B-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, Suprathermal Ion Spectrograph B Telescope, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_EPD-STEP-RATES: Solar Orbiter, Level 2 Low Latency, Energetic Particle Detector, SupraThermal Electrons and Protons, Particle Rates - J. Rodriguez-Pacheco (Space Research Group, Universidad de Alcala)
SOLO_LL02_MAG: Solar Orbiter Level 2 Low Latency Magnetometer Data - T. Horbury (The Blackett Laboratory, Imperial College London)
SOLO_LL02_RPW-SBM1: Solar Orbiter Radio/Plasma Wave, LL02 parameters - M. Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_LL02_RPW-SBM2: Solar Orbiter Radio/Plasma Wave, LL02 parameters - M. Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_LL02_RPW-TNR: Solar Orbiter Radio/Plasma Wave, LL02 parameters - M. Maksimovic (LESIA, Observatoire de Paris-CNRS)
SOLO_LL02_SWA-EAS-SS: SWA-EAS Low Latency LL02 Data - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_LL02_SWA-HIS-RAT: SWA-HIS LL02 Ratios and Spectra - C. J. Owen (MSSL-UCL, University College London, UK)
SOLO_LL02_SWA-PAS-MOM: SWA-PAS Quick Look Moments - C. J. Owen (MSSL-UCL, University College London, UK)
SO_AT_DEF: SOHO Definitive Attitude Data
SO_K0_CEL: SOHO Charge, Element and Isotope Analysis System, Key Parameters - Peter Bochsler (Physikalisches Institut, )
SO_K0_CST: SOHO ComprehensiveSuprathermal and EnergeticParticle Analyser - Horst Kunow (University of Kiel, Germany)
SO_K0_ERN: SOHO Energetic and Relativistic Nuclei and Electron experiment, Key Parameters - J Torsti (University of Turku)
SO_OR_DEF: SOHO Definitive Orbit Data
SO_OR_PRE: Soho Predicted Data Orbit
ST5-094_1SEC_MAG: Magnetometer>3 component magnetic field from miniature tri-axial magnetometer. - Delores Knipp (University of Colorado, Boulder)
ST5-155_1SEC_MAG: Magnetometer>3 component magnetic field from miniature tri-axial magnetometer. - Delores Knipp (University of Colorado, Boulder)
ST5-224_1SEC_MAG: Magnetometer>3 component magnetic field from miniature tri-axial magnetometer. - Delores Knipp (University of Colorado, Boulder)
STA_COHO1HR_MERGED_MAG_PLASMA: Merged hourly magnetic field, plasma, proton fluxes, and ephermis data - Natasha Papitashvili (NASA/GSFC)
STA_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
STA_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
STA_L1_HET: STEREO Ahead IMPACT/HET Level 1 Data - J. Luhmann (UCB/SSL)
STA_L1_IMPACT_BURST: STEREO Ahead IMPACT Burst Criteria - J. Luhmann (UCB/SSL)
STA_L1_IMPACT_HKP: STEREO Ahead IMPACT State of Health - J. Luhmann (UCB/SSL)
STA_L1_LET: STEREO Ahead IMPACT/LET Level 1 Data. - J. Luhmann (UCB/SSL)
STA_L1_MAGB_RTN: STEREO Ahead IMPACT/MAG Magnetic Field Vectors - Christina Lee (UCB/SSL)
STA_L1_MAGB_SC: STEREO Ahead IMPACT/MAG Magnetic Field Vectors - Christina Lee (UCB/SSL)
STA_L1_MAG_RTN: STEREO Ahead IMPACT/MAG Magnetic Field Vectors - Christina Lee (UCB/SSL)
STA_L1_MAG_SC: STEREO Ahead IMPACT/MAG Magnetic Field Vectors - Christina Lee (UCB/SSL)
STA_L1_SEPT: STEREO Ahead IMPACT/SEPT Level 1 Data - J. Luhmann (UCB/SSL)
STA_L1_SIT: STEREO Ahead IMPACT/SIT Level 1 Data - J. Luhmann (UCB/SSL)
STA_L1_STE: STEREO Ahead IMPACT/STE Spectra - J. Luhmann (UCB/SSL)
STA_L1_SWEA_DISB: STEREO Ahead IMPACT/SWEA 3D Burst Mode Distributions - J. Luhmann (UCB/SSL)
STA_L1_SWEA_DIST: STEREO Ahead IMPACT/SWEA 3D Distributions - J. Luhmann (UCB/SSL)
STA_L1_SWEA_SPEC: STEREO Ahead IMPACT/SWEA Spectra - J. Luhmann (UCB/SSL)
STA_L2_MAGPLASMA_1M: STEREO Ahead IMPACT/MAG Magnetic Field and PLASTIC Solar Wind Plasma Data - Christina Lee (UCB/SSL)
STA_L2_PLA_1DMAX_10MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_PLA_1DMAX_1HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_PLA_1DMAX_1MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_PLA_ALPHA_RA_1DMAX_10MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_PLA_ALPHA_RA_1DMAX_1HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_PLA_IRON_Q_2HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L2_SWEA_PAD: STEREO Ahead IMPACT SWEA Pitch Angle Distribution - J. Luhmann (UC Berkeley Space Sciences Laboratory)
STA_L3_PLA_HE2PL_F_VSW_01HR: He++ Phase Space Density (PSD) Binned by V/Vsw. - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_PLA_HEPLUS_24HR: He+ Fluxes Binned by V/Vsw, STEREO/PLASTIC Level 3 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_PLA_HEPLUS_F_VSW_01HR: He+ Phase Space Density (PSD) Binned by V/Vsw. - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_PLA_HEPLUS_F_VSW_10MIN: He+ Phase Space Density (PSD) Binned by V/Vsw. - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_PLA_HEPLUS_F_VSW_24HR: He+ Phase Space Density (PSD) Binned by V/Vsw, STEREO/PLASTIC Level 3 - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_PLA_HEPLUS_SW_VELCTDIST_5MIN: He+ SW Frame Velocity Count Distributions. - Dr. Antoinette Galvin (University of New Hampshire)
STA_L3_WAV_HFR: STEREO-A/WAVES/HFR Data - Milan Maksimovic (milan.maksimovic@obspm.fr) and Stuart D. Bale (bale@berkeley.edu) (LESIA, Observatoire de Paris-PSL, CNRS and UC Berkeley Space Sciences Laboratory)
STA_L3_WAV_LFR: STEREO-A/WAVES/LFR Data - Milan Maksimovic (milan.maksimovic@obspm.fr) and Stuart D. Bale (bale@berkeley.edu) (LESIA, Observatoire de Paris-PSL, CNRS and UC Berkeley Space Sciences Laboratory)
STA_LB_IMPACT: STEREO Ahead IMPACT Beacon Data - J. Luhmann (UCB/SSL)
STA_LB_MAG_RTN: STEREO Ahead IMPACT/MAG Magnetic Field Vectors - J. Luhmann (UCB/SSL)
STA_LB_PLA_BROWSE: STEREO/PLASTIC Beacon Proton Parameters [PRELIM] - Dr. Antoinette Galvin (University of New Hampshire)
STB_COHO1HR_MERGED_MAG_PLASMA: Merged hourly magnetic field, plasma, proton fluxes, and ephermis data - Natasha Papitashvili (NASA/GSFC)
STB_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
STB_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
STB_L1_HET: STEREO Behind IMPACT/HET Level 1 Data - J. Luhmann (UCB/SSL)
STB_L1_IMPACT_BURST: STEREO Ahead IMPACT Burst Criteria - J. Luhmann (UCB/SSL)
STB_L1_IMPACT_HKP: STEREO Behind IMPACT State of Health - J. Luhmann (UCB/SSL)
STB_L1_LET: STEREO Behind IMPACT/LET Level 1 Data. - J. Luhmann (UCB/SSL)
STB_L1_MAGB_RTN: STEREO Behind IMPACT/MAG Magnetic Field Vectors - J. Luhmann (UCB/SSL)
STB_L1_MAGB_SC: STEREO Behind IMPACT/MAG Magnetic Field Vectors - J. Luhmann (UCB/SSL)
STB_L1_MAG_RTN: STEREO Behind IMPACT/MAG Magnetic Field Vectors - J. Luhmann (UCB/SSL)
STB_L1_MAG_SC: STEREO Behind IMPACT/MAG Magnetic Field Vectors - J. Luhmann (UCB/SSL)
STB_L1_SEPT: STEREO Ahead IMPACT/SEPT Level 1 Data - J. Luhmann (UCB/SSL)
STB_L1_SIT: STEREO Behind IMPACT/SIT Level 1 Data - J. Luhmann (UCB/SSL)
STB_L1_STE: STEREO Behind IMPACT/STE Spectra - J. Luhmann (UCB/SSL)
STB_L1_SWEA_DISB: STEREO Ahead IMPACT/SWEA 3D Burst Mode Distributions - J. Luhmann (UCB/SSL)
STB_L1_SWEA_DIST: STEREO Ahead IMPACT/SWEA 3D Distributions - J. Luhmann (UCB/SSL)
STB_L1_SWEA_SPEC: STEREO Ahead IMPACT/SWEA Spectra - J. Luhmann (UCB/SSL)
STB_L2_MAGPLASMA_1M: STEREO Behind IMPACT/MAG Magnetic Field and PLASTIC Solar Wind Plasma Data - Christina Lee (UCB/SSL)
STB_L2_PLA_1DMAX_10MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_PLA_1DMAX_1HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_PLA_1DMAX_1MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_PLA_ALPHA_RA_1DMAX_10MIN: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_PLA_ALPHA_RA_1DMAX_1HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_PLA_IRON_Q_2HR: STEREO/PLASTIC Level 2 - Dr. Antoinette Galvin (University of New Hampshire)
STB_L2_SWEA_PAD: STEREO Behind IMPACT SWEA Pitch Angle Distribution - J. Luhmann (UC Berkeley Space Sciences Laboratory)
STB_L3_WAV_HFR: STEREO-B/WAVES/HFR Data - Milan Maksimovic (milan.maksimovic@obspm.fr) and Stuart D. Bale (bale@berkeley.edu) (LESIA, Observatoire de Paris-PSL, CNRS and UC Berkeley Space Sciences Laboratory)
STB_L3_WAV_LFR: STEREO-B/WAVES/LFR Data - Milan Maksimovic (milan.maksimovic@obspm.fr) and Stuart D. Bale (bale@berkeley.edu) (LESIA, Observatoire de Paris-PSL, CNRS and UC Berkeley Space Sciences Laboratory)
STB_LB_IMPACT: STEREO Ahead IMPACT Beacon Data - J. Luhmann (UCB/SSL)
STB_LB_PLA_BROWSE: STEREO/PLASTIC Beacon Proton Parameters [PRELIM] - Dr. Antoinette Galvin (University of New Hampshire)
STEREO_LEVEL2_SWAVES: STEREO WAVES (SWAVES) Radio Intensity Spectra, both Ahead and Behind s/c - M. Kaiser (NASA/GSFC)
STEREO_WAVES_R0_GIFWALK: Links to STEREO pre-generated daily summary plots (png, pdf and ps files) - M. Kaiser (NASA GSFC)
STPSAT-6_FALCON_SEED-L1: STPSat-6 Electron Detector & Dosimeter - G. McHarg (United States Air Force Academy)
SUISEI_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SUISEI_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
SX_K0_30F: 30-s averaged fluxes: 4 Instruments - Glenn Mason (U. Maryland )
SX_K0_POF: SAMPEX POLARCAP Averages: 4 Instruments - G.MASON (U.MD )
THAPRED_OR_SSC: THEMIS-A Predicted Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THA_L1_STATE: Probe state file, contains position, attitude, sun pulse data - V. Angelopoulos (UCB, NASA NAS5-02099)
THA_L2_EFI: Spacecraft-collected (EFI) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THA_L2_EFP: Spacecraft-collected Particle Burst (EFP) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THA_L2_EFW: Spacecraft-collected Wave Burst (EFW) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THA_L2_ESA: THEMIS-A: Electrostatic Analyzer (ESA): Electron/Ion Ground-Calculated Energy Fluxes (ions: 5 eV to 25 keV) electrons: 6 eV to 30 keV) and Moments (density, velocity, pressure, and temperature). Includes FULL, REDUCED and BURST modes. FULL: high angular resolution, low (few min) time resolution. REDUCED: degraded angular resolution, high (approx. 3 sec) time resolution. BURST: high angular resolution, high time resolution; only short bursts of data. Note that angular resolution affects moments since they are obtained integrating over the mode-specific angular distribution. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THA_L2_FBK: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board- digitally computed Filter Bank spectra and E12 peak and average in HF band. - V. Angelopoulos, J. W. Bonnell & F. S. Mozer; A. Roux and R. E. Ergun (UCB; CETP and LASP respectively, NASA NAS5-02099)
THA_L2_FFT: THEMIS-A: On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field, for particle and wave burst survey modes. - V. Angelopoulos (UCB, NASA NAS5-02099)
THA_L2_FGM: Spacecraft-collected fluxgate magnetometer, Decimated TeleMetry High, DSL, GSE and GSM coordinates - V. Angelopoulos, U. Auster & K.H. Glassmeier and W. Baumjohann (UCB, TUBS and IWF respectively, NASA NAS5-02099)
THA_L2_FIT: THEMIS-A: On Board spin fits of Electric (EFI) and Magnetic (FGM) field. - V. Angelopoulos (UCB, NASA NAS5-02099)
THA_L2_GMOM: THEMIS-A: Solid State Telescope (ESA+SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (ions: 5 eV - 4 MeV,electrons: 6 eV - 700 keV) - V. Angelopoulos, D. Larson & R.P. Lin, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THA_L2_MOM: THEMIS-A: On Board moments: Electron/Ion moments density, flux, velocity, pressure and temperature. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THA_L2_SCM: Spacecraft-collected search-coil magnetometer (SCM) Magnetic field - V. Angelopoulos, A. Roux and O. LeContel (UCB, LPP NASA NAS5-02099)
THA_L2_SST: THEMIS-A: Solid State Telescope (SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (30 keV - 300 keV). - V. Angelopoulos, D. Larson & R.P. Lin (UCB, NASA NAS5-02099)
THA_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THBPRED_OR_SSC: THEMIS-B Predicted Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THB_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
THB_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
THB_L1_STATE: Probe state file, contains position, attitude, sun pulse data - V. Angelopoulos (UCB, NASA NAS5-02099)
THB_L2_EFI: Spacecraft-collected (EFI) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THB_L2_EFP: Spacecraft-collected Particle Burst (EFP) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THB_L2_EFW: Spacecraft-collected Wave Burst (EFW) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THB_L2_ESA: THEMIS-B: Electrostatic Analyzer (ESA): Electron/Ion Ground-Calculated Energy Fluxes (ions: 5 eV to 25 keV) electrons: 6 eV to 30 keV) and Moments (density, velocity, pressure, and temperature). Includes FULL, REDUCED and BURST modes. FULL: high angular resolution, low (few min) time resolution. REDUCED: degraded angular resolution, high (approx. 3 sec) time resolution. BURST: high angular resolution, high time resolution; only short bursts of data. Note that angular resolution affects moments since they are obtained integrating over the mode-specific angular distribution. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THB_L2_FBK: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board- digitally computed Filter Bank spectra and E12 peak and average in HF band. - V. Angelopoulos, J. W. Bonnell & F. S. Mozer; A. Roux and R. E. Ergun (UCB; CETP and LASP respectively, NASA NAS5-02099)
THB_L2_FFT: THEMIS-B: On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field, for particle and wave burst survey modes. - V. Angelopoulos (UCB, NASA NAS5-02099)
THB_L2_FGM: Spacecraft-collected fluxgate magnetometer, Decimated TeleMetry High, DSL, GSE and GSM coordinates - V. Angelopoulos, U. Auster & K.H. Glassmeier and W. Baumjohann (UCB, TUBS and IWF respectively, NASA NAS5-02099)
THB_L2_FIT: THEMIS-B: On Board spin fits of Electric (EFI) and Magnetic (FGM) field. - V. Angelopoulos (UCB, NASA NAS5-02099)
THB_L2_GMOM: THEMIS-B: Solid State Telescope (ESA+SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (ions: 5 eV - 4 MeV,electrons: 6 eV - 700 keV) - V. Angelopoulos, D. Larson & R.P. Lin, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THB_L2_MERGED: This data set contains ARTEMIS P1(THEMIS B) plasma parameters from the Electrostatic Analyzer (ESA), magnetic field data from the FGM instrument, and geocentric and selenocentric spacecraft position data. The data are at 96s or 384s resolution. For more details see - N. Papatashvilli, J.H. King (SPDF, NASA/GSFC)
THB_L2_MOM: THEMIS-B: On Board moments: Electron/Ion moments density, flux, velocity, pressure and temperature. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THB_L2_SCM: Spacecraft-collected search-coil magnetometer (SCM) Magnetic field - V. Angelopoulos, A. Roux and O. LeContel (UCB, LPP NASA NAS5-02099)
THB_L2_SST: THEMIS-B: Solid State Telescope (SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (30 keV - 300 keV). - V. Angelopoulos, D. Larson & R.P. Lin (UCB, NASA NAS5-02099)
THB_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THCPRED_OR_SSC: THEMIS-C Predicted Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THC_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
THC_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
THC_L1_STATE: Probe state file, contains position, attitude, sun pulse data - V. Angelopoulos (UCB, NASA NAS5-02099)
THC_L2_EFI: Spacecraft-collected (EFI) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THC_L2_EFP: Spacecraft-collected Particle Burst (EFP) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THC_L2_EFW: Spacecraft-collected Wave Burst (EFW) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THC_L2_ESA: THEMIS-C: Electrostatic Analyzer (ESA): Electron/Ion Ground-Calculated Energy Fluxes (ions: 5 eV to 25 keV) electrons: 6 eV to 30 keV) and Moments (density, velocity, pressure, and temperature). Includes FULL, REDUCED and BURST modes. FULL: high angular resolution, low (few min) time resolution. REDUCED: degraded angular resolution, high (approx. 3 sec) time resolution. BURST: high angular resolution, high time resolution; only short bursts of data. Note that angular resolution affects moments since they are obtained integrating over the mode-specific angular distribution. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THC_L2_FBK: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board- digitally computed Filter Bank spectra and E12 peak and average in HF band. - V. Angelopoulos, J. W. Bonnell & F. S. Mozer; A. Roux and R. E. Ergun (UCB; CETP and LASP respectively, NASA NAS5-02099)
THC_L2_FFT: THEMIS-C: On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field, for particle and wave burst survey modes. - V. Angelopoulos (UCB, NASA NAS5-02099)
THC_L2_FGM: Spacecraft-collected fluxgate magnetometer, Decimated TeleMetry High, DSL, GSE and GSM coordinates - V. Angelopoulos, U. Auster & K.H. Glassmeier and W. Baumjohann (UCB, TUBS and IWF respectively, NASA NAS5-02099)
THC_L2_FIT: THEMIS-C: On Board spin fits of Electric (EFI) and Magnetic (FGM) field. - V. Angelopoulos (UCB, NASA NAS5-02099)
THC_L2_GMOM: THEMIS-C: Solid State Telescope (ESA+SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (ions: 5 eV - 4 MeV,electrons: 6 eV - 700 keV) - V. Angelopoulos, D. Larson & R.P. Lin, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THC_L2_MERGED: This data set contains ARTEMIS P2(THEMIS C) plasma parameters from the Electrostatic Analyzer (ESA), magnetic field data from the FGM instrument, and geocentric and selenocentric spacecraft position data. The data are at 96s or 384s resolution. For more details see - N. Papatashvilli, J.H. King (SPDF, NASA/GSFC)
THC_L2_MOM: THEMIS-C: On Board moments: Electron/Ion moments density, flux, velocity, pressure and temperature. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THC_L2_SCM: Spacecraft-collected search-coil magnetometer (SCM) Magnetic field - V. Angelopoulos, A. Roux and O. LeContel (UCB, LPP NASA NAS5-02099)
THC_L2_SST: THEMIS-C: Solid State Telescope (SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (30 keV - 300 keV). - V. Angelopoulos, D. Larson & R.P. Lin (UCB, NASA NAS5-02099)
THC_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THDPRED_OR_SSC: THEMIS-D Predicted Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THD_L1_STATE: Probe state file, contains position, attitude, sun pulse data - V. Angelopoulos (UCB, NASA NAS5-02099)
THD_L2_EFI: Spacecraft-collected (EFI) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THD_L2_EFP: Spacecraft-collected Particle Burst (EFP) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THD_L2_EFW: Spacecraft-collected Wave Burst (EFW) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THD_L2_ESA: THEMIS-D: Electrostatic Analyzer (ESA): Electron/Ion Ground-Calculated Energy Fluxes (ions: 5 eV to 25 keV) electrons: 6 eV to 30 keV) and Moments (density, velocity, pressure, and temperature). Includes FULL, REDUCED and BURST modes. FULL: high angular resolution, low (few min) time resolution. REDUCED: degraded angular resolution, high (approx. 3 sec) time resolution. BURST: high angular resolution, high time resolution; only short bursts of data. Note that angular resolution affects moments since they are obtained integrating over the mode-specific angular distribution. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THD_L2_FBK: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board- digitally computed Filter Bank spectra and E12 peak and average in HF band. - V. Angelopoulos, J. W. Bonnell & F. S. Mozer; A. Roux and R. E. Ergun (UCB; CETP and LASP respectively, NASA NAS5-02099)
THD_L2_FFT: THEMIS-D: On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field, for particle and wave burst survey modes. - V. Angelopoulos (UCB, NASA NAS5-02099)
THD_L2_FGM: Spacecraft-collected fluxgate magnetometer, Decimated TeleMetry High, DSL, GSE and GSM coordinates - V. Angelopoulos, U. Auster & K.H. Glassmeier and W. Baumjohann (UCB, TUBS and IWF respectively, NASA NAS5-02099)
THD_L2_FIT: THEMIS-D: On Board spin fits of Electric (EFI) and Magnetic (FGM) field. - V. Angelopoulos (UCB, NASA NAS5-02099)
THD_L2_GMOM: THEMIS-D: Solid State Telescope (ESA+SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (ions: 5 eV - 4 MeV,electrons: 6 eV - 700 keV) - V. Angelopoulos, D. Larson & R.P. Lin, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THD_L2_MOM: THEMIS-D: On Board moments: Electron/Ion moments density, flux, velocity, pressure and temperature. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THD_L2_SCM: Spacecraft-collected search-coil magnetometer (SCM) Magnetic field - V. Angelopoulos, A. Roux and O. LeContel (UCB, LPP NASA NAS5-02099)
THD_L2_SST: THEMIS-D: Solid State Telescope (SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (30 keV - 300 keV). - V. Angelopoulos, D. Larson & R.P. Lin (UCB, NASA NAS5-02099)
THD_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THEMIS_R0_EFI: THEMIS A/B/C/D/E Electric Field Instrument (EFI) Waveform Level-1 Products - V. Angelopoulos (UCB, NASA NAS5-02099)
THEMIS_R0_GIFWALK: Links to THEMIS pre-generated MP Crossing Survey plots - David Sibeck (NASA GSFC)
THEMIS_R0_GMAG: THEMIS GMAG Reprocesses http://cdaweb.gsfc.nasa.gov/THEMIS_GMAG_Processing_History.doc - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THEPRED_OR_SSC: THEMIS-E Predicted Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THE_L1_STATE: Probe state file, contains position, attitude, sun pulse data - V. Angelopoulos (UCB, NASA NAS5-02099)
THE_L2_EFI: Spacecraft-collected (EFI) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THE_L2_EFP: Spacecraft-collected Particle Burst (EFP) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THE_L2_EFW: Spacecraft-collected Wave Burst (EFW) Electric field - V. Angelopoulos, J. Bonnell & F. Mozer (UCB, NASA NAS5-02099)
THE_L2_ESA: THEMIS-E: Electrostatic Analyzer (ESA): Electron/Ion Ground-Calculated Energy Fluxes (ions: 5 eV to 25 keV) electrons: 6 eV to 30 keV) and Moments (density, velocity, pressure, and temperature). Includes FULL, REDUCED and BURST modes. FULL: high angular resolution, low (few min) time resolution. REDUCED: degraded angular resolution, high (approx. 3 sec) time resolution. BURST: high angular resolution, high time resolution; only short bursts of data. Note that angular resolution affects moments since they are obtained integrating over the mode-specific angular distribution. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THE_L2_FBK: Probe Electric Field Instrument and Search Coil Magnetometer Instrument, Digital Fields Board- digitally computed Filter Bank spectra and E12 peak and average in HF band. - V. Angelopoulos, J. W. Bonnell & F. S. Mozer; A. Roux and R. E. Ergun (UCB; CETP and LASP respectively, NASA NAS5-02099)
THE_L2_FFT: THEMIS-E: On Board Fast Fourier Transform (FFT) power spectra of Electric (EFI) and Magnetic (SCM) field, for particle and wave burst survey modes. - V. Angelopoulos (UCB, NASA NAS5-02099)
THE_L2_FGM: Spacecraft-collected fluxgate magnetometer, Decimated TeleMetry High, DSL, GSE and GSM coordinates - V. Angelopoulos, U. Auster & K.H. Glassmeier and W. Baumjohann (UCB, TUBS and IWF respectively, NASA NAS5-02099)
THE_L2_FIT: THEMIS-E: On Board spin fits of Electric (EFI) and Magnetic (FGM) field. - V. Angelopoulos (UCB, NASA NAS5-02099)
THE_L2_GMOM: THEMIS-E: Solid State Telescope (ESA+SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (ions: 5 eV - 4 MeV,electrons: 6 eV - 700 keV) - V. Angelopoulos, D. Larson & R.P. Lin, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THE_L2_MOM: THEMIS-E: On Board moments: Electron/Ion moments density, flux, velocity, pressure and temperature. - V. Angelopoulos, C.W. Carlson & J. McFadden (UCB, NASA NAS5-02099)
THE_L2_SCM: Spacecraft-collected search-coil magnetometer (SCM) Magnetic field - V. Angelopoulos, A. Roux and O. LeContel (UCB, LPP NASA NAS5-02099)
THE_L2_SST: THEMIS-E: Solid State Telescope (SST): Energy Flux spectrogram: Data includes: Electron/Ion Ground-Calculated Fluxes (30 keV - 300 keV). - V. Angelopoulos, D. Larson & R.P. Lin (UCB, NASA NAS5-02099)
THE_OR_SSC: Orbit parameters from SSCWeb - SSCWeb (SPDF/Goddard)
THG_L1_ASK: Ground-based All Sky Imager (ASI), 3sec S-N Keograms, THEMIS GBO network - V. Angelopoulos, S. Mende & E. Donovan (UCB & Univ of Calgary respectively, NASA NAS5-02099)
THG_L2_MAG_NRSQ: Ground-based Vector Magnetic Field at Narsarsuaq, Greenland, 20 sec time Resolution. - Hans Gleisner (Geomagnetism & Remote Sensing, Danish Meteorological Institute, Lyngbyvej 100, DK-2100 Copenhagen. email: hgl@dmi.dk)
THG_R0_ASI: THEMIS Ground-Based All Sky Imager (ASI) Level-0 Image Data links - V. Angelopoulos (UCB, NASA NAS5-02099)
TIMED_EDP_GUVI: Electron Density Profiles - Andrew Christensen (Aerospace)
TIMED_L1BV20_SABER: IR Radiances in 10 channels (1.27 to 17ym) from 0 to 150 km, Version 1.07, - James Russell III (Hampton University)
TIMED_L1CDISK_GUVI: Airglow fluxes at 5 wavelengths bands - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1216A_MERC_MOVIES: Airglow flux 14 day movies, at wavelength 1216A in Mercator Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1216A_NP_MOVIES: Airglow flux 14 day movies, at wavelength 1216 A in North Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1216A_SP_MOVIES: Airglow flux 14 day movies, at wavelength 1216 A in South Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1304A_MERC_MOVIES: Airglow flux 14 day movies, at wavelength 1304A in Mercator Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1304A_NP_MOVIES: Airglow flux 14 day movies, at wavelength 1304A in North Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1304A_SP_MOVIES: Airglow flux 14 day movies, at wavelength 1304A in South Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1356A_MERC_MOVIES: Airglow flux 14 day movies, at wavelength 1356A in Mercator Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1356A_NP_MOVIES: Airglow flux 14 day movies, at wavelength 1356A in North Polar Pojection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_1356A_SP_MOVIES: Airglow flux 14 day movies, at wavelength 1356A in South Polar Pojection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH1_MERC_MOVIES: Airglow flux 14 day movies, at wavelength LBH1 in Mercator Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH1_NP_MOVIES: Airglow flux 14 day movies, at wavelength LBH1 in North Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH1_SP_MOVIES: Airglow flux 14 day movies, at wavelength LBH1 in South Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH2_MERC_MOVIES: Airglow flux 14 day movies, at wavelength LBH2 in Mercator Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH2_NP_MOVIES: Airglow flux 14 day movies, at wavelength LBH2 in North Polar Projection - Andrew Christensen (Aerospace)
TIMED_L1CDISK_GUVI_LBH2_SP_MOVIES: Airglow flux 14 day movies, at wavelength LBH2 in South Polar Projection - Andrew Christensen (Aerospace)
TIMED_L2A_SABER: O3, CO2, H2O Mixing Ratios and O, O2, OH, NO Volume Emission Rates, also NMC Neutral Temp., Density, and Pressure, Version 2.0, - James Russell III (Hampton University)
TIMED_L3A_SEE: Solar irradiances 0.1 - 194 nm, Version 11 - Tom Woods (LASP/CU)
TIMED_WINDVECTORSNCAR_TIDI: Zonal and meridional winds at 60 to 180 km, version 0307, - Timothy Killeen (NCAR)
TOOWINDY_E_NE: Electron density and electric field measurements during the rocket flight. - D. Hysell (Cornell University)
TSS-1R_M1_CSAA: TSS-1R, Shuttle Attitude Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSAB: TSS-1R, Orbiter and Target State Vectors IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSCA: TSS-1R, Computed OA Data Values IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSCB: TSS-1R, Special Computation Events IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSEA: TSS-1R, Temperature, Voltage, and Current Measurements IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSEB: TSS-1R, Supply and Waste Water Quantities IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSMA: TSS-1R, KU-Band Communications/RADAR Roll and Pitch Monitors IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSMB: TSS-1R, KU-Band Communications/RADAR Power and Range Monitors IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSSA: TSS-1R, FCP, Water and Waste Dump, FES, and Power Status IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSSB: TSS-1R, KU-BAND Communications/RADAR and Recorder Operation Status IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSSC: TSS-1R, RCS/Vernier Jets-Impulse/Exhaust Gases Status IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_CSTA: TSS-1R, GMT and MET Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_DBPO: TSS-1R, Boom Tip Position (DBPO) IDFS format - Jean Sabbagh (ASI)
TSS-1R_M1_DBSA: TSS-1R, Boom, DPY/RTR, and JTS Status Data (DBSA) IDFS format - Jean Sabbagh (ASI)
TSS-1R_M1_DBSB: TSS-1R, Boom Stowed Status, DPY/RTR Status, and JTR Fire Status IDFS format - Jean Sabbagh (ASI)
TSS-1R_M1_DBSC: TSS-1R, DPY/RTR and JTR Power Status IDFS format - Jean Sabbagh (ASI)
TSS-1R_M1_DBTA: TSS-1R, Boom Temperature Monitors (DBTA) IDFS format - Jean Sabbagh (ASI)
TSS-1R_M1_DCDV: TSS-1R, DV Voltage and DVG Pressure Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCGA: TSS-1R, Electron Gun Current Monitors (DCGA) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCGB: TSS-1R, Electron Gun Tether Current Offset Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCGC: TSS-1R, Electron Filament Voltage And Acceleration Potentials IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCMA: TSS-1R, General Monitor Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCMB: TSS-1R, Memory Dump Data IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCMC: TSS-1R, EGA Filament and Tether Current Cycle Data IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCMD: TSS-1R, DCORE Format Counter and Dump Data IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCME: TSS-1R, Applicative Programs Data IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCSA: TSS-1R, General High Rate Status Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCSB: TSS-1R, General Status Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DCTA: TSS-1R, Temperature Measurements IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_DPHA: TSS-1R, 16/major Frame Miscellaneous Housekeeping Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPHB: TSS-1R, SFMSD Command Word Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPHC: TSS-1R, Rotating Memeory Dump Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPHD: TSS-1R, Segment Information IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPHE: TSS-1R, Time Stamp Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMA: TSS-1R, CP Tether Tensions IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMB: TSS-1R, Low Rate Tether Information IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMC: TSS-1R, 16 bit Measured Tether Lengths and Rates IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMD: TSS-1R, Tether Rate Raw Timer Counts IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPME: TSS-1R, Miscellaneous Tether Measurements IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMF: TSS-1R, Voltage, Current, and Tether Tension Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMG: TSS-1R, Tether Length IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMH: TSS-1R, Tether Velocity IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMI: TSS-1R, Tether Length Raw Encoder Counts IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMJ: TSS-1R, DEL-L Measurements IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPMK: TSS-1R, Reel Motor Command Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSA: TSS-1R, Boom Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSC: TSS-1R, Power and ADC Voltage Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSD: TSS-1R, Latch Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSE: TSS-1R, U1 and U2 Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSF: TSS-1R, L-DOT, DEL-L, and Talkback Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSG: TSS-1R, 1/major Frame Miscellaneous Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSH: TSS-1R, 16/major Frame Miscellaneous Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSI: TSS-1R, Maneuver Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPSJ: TSS-1R, Miscellaneous Relay Status Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPTA: TSS-1R, Reel And Boom Temperature Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_DPTB: TSS-1R, Temperature Data IDFS format - Ron Geiger (Martin Marietta Astronautics)
TSS-1R_M1_EPMA: TSS-1R, Temperature, Voltage, Current, and Freon Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPMB: TSS-1R, Output Command Block and Variable Data Block IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPMC: TSS-1R, SFMDM Last Command Accepted Buffer IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPMF: TSS-1R, Timeline Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPMG: TSS-1R, DDCS and SFMDM Miscellaneous Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPMH: TSS-1R, SFMDM RS-422 And IO Transfer Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPSA: TSS-1R, EMP Satellite and Deployer Status Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPSB: TSS-1R, EMP SFMDM General Status Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPSC: TSS-1R, EMP SFMDM D05 and D28 LEV and PUL Status Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_EPSD: TSS-1R, SDIO Channel Status Data IDFS format - Tony Lavoie (Marshall Space Flight Center)
TSS-1R_M1_RPBB: TSS-1R, Boom Biasing Current and Voltage IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPDM: TSS-1R, DIFP Peak Monitor Data (RPDM) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPDP: TSS-1R, DIFP Deflection and Retard Data (RPDP) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPEA: TSS-1R, Satellite Mounted Electron Sensors (RPEA) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPEB: TSS-1R, Boom Mounted Electron Sensors IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPEM: TSS-1R, DIFP Electrometer Data IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPHA: TSS-1R, DIFP Miscellaneous Housekeeping (RPHA) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPHB: TSS-1R, DIFP A/D Voltage And Current Monitors IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPHC: TSS-1R, SPES Voltage And Current Monitors (RPHC) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPHD: TSS-1R, SPES Grid Voltages (RPHD) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPHE: TSS-1R, ROPE CEP and FS Voltage And Temperature Monitors (RPHE) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPHF: TSS-1R, Satellite Programmable Power Supply Monitors (RPHF) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPHG: TSS-1R, Floating Power Supply Current (RPHG) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPIA: TSS-1R, Satellite Mounted Ion Sensor IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPIB: TSS-1R, Boom Mounted Ion Sensors (RPIB) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPSA: TSS-1R, SPES Grid Bias And HVU 1/2 Status (RPSA) IDFS format - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_M1_RPSB: TSS-1R, ROPE Command Status Words (RPSB) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPSC: TSS-1R, Floating Supply Discrete Status Values (RPSC) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RPSD: TSS-1R, DIFP RAM Test Data (RPSD) IDFS format - Dr. Nobie Stone (Marshall Space Flight Center)
TSS-1R_M1_RTEF: TSS-1R, Langmuir Probe DC Electric Field Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTHF: TSS-1R, High Frequency Electromagnetic Wave Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTIP: TSS-1R, Ion Probe Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKA: TSS-1R, AC Housekeeping measurements IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKC: TSS-1R, Error table measurements IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKD: TSS-1R, Telecommand Echo IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKE: TSS-1R, Pentode Current And DCBP Voltage IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKF: TSS-1R, RETE Format Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKG: TSS-1R, LF RETE Format Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKH: TSS-1R, MF RETE Format Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTKI: TSS-1R, HF RETE Format Data IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTLA: TSS-1R, Low Frequency Electromagnetic Wave Data (Band A) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTLB: TSS-1R, Low Frequency Electromagnetic Wave Data (Band B) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTMC: TSS-1R, Medium Frequency Electromagnetic Wave Data (Band C) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTMD: TSS-1R, Medium Frequency Electromagnetic Wave Data (Band D) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTME: TSS-1R, Medium Frequency Electromagnetic Wave Data (Band E) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTMF: TSS-1R, Medium Frequency Electromagnetic Wave Data (Band F) IDFS format - Dr. Marino Dobrowolny (Instituto Di Fisica Dello Spazio Interplanetario)
TSS-1R_M1_RTRLP: TSS-1R, Reduced Langmuir Probe Data IDFS format - J-P. Lebreton (ESA/ESTEC, Solar System Division)
TSS-1R_M1_SCAC: TSS-1R, SLA vector coarse acceleration (SCAC) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCAF: TSS-1R, SLA High Res Vector Acceleration Measurements (SCAF) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCMA: TSS-1R, SLA Temperature and Voltage Monitors IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCMB: TSS-1R, SA Temperature and Overtemperature Monitors (SCMB) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCMC: TSS-1R, Satellite Ampmeter Current Monitors (SCMC) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCSA: TSS-1R, Low time resolution experiment status flags (SCSA) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SCSB: TSS-1R, High time resolution experiment status flags (SCSB) IDFS format - Carlo Bonifazi (ASI)
TSS-1R_M1_SHAA: TSS-1R, Yaw, Roll and Pitch Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAB: TSS-1R, Scaled Roll, Yaw and Pitch Data (SHAB) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAC: TSS-1R, Gyro Rate and Sun Presence IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAD: TSS-1R, Gyro Angular Data (SHAD) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAE: TSS-1R, Gyro and Attitude Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAF: TSS-1R, Satellite Spin Rate (SAHF) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHAG: TSS-1R, Gyro and Attitude Angular Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHA: TSS-1R, Miscellaneous Housekeeping Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHB: TSS-1R, 24 Bit Battery Current and Power Moniters (SHHB) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHC: TSS-1R, Miscellaneous Timing Data (SHHC) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHD: TSS-1R, Various 64/major frame 8 bit Housekeeping Data (SHHD) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHE: TSS-1R, Low time resolution 3 bit satellite monitors (SHHE) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHHF: TSS-1R, Satellite RX Coherent AGC and Loop Stress Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHMA: TSS-1R, Onboard Data Handling RSMN Data (SHMA) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHMB: TSS-1R, Onboard Data Handling ASMN Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHMC: TSS-1R, Memory Dump And TLC Data (SHMC) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHMD: TSS-1R, OBDH And AMCS Status Flags IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHME: TSS-1R, OBDH and AMCS Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHPA: TSS-1R, Satellite miscellaneous power monitors IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSA: TSS-1R, Low resolution gyro status flags (SHSA) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSB: TSS-1R, Gyro converter, heating and wheel status data (SHSB) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSC: TSS-1R, Low resolution FDS3/FDS4 status flags (SHSC) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSD: TSS-1R, Satellite Program Status Flags IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSE: TSS-1R, Medium resolution miscellaneous status flags (SHSE) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSF: TSS-1R, Satellite medium resolution status data (SHSF) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSG: TSS-1R, Satellite slow status data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSH: TSS-1R, Satellite high time resolution status data (SHSH) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSI: TSS-1R, Satellite miscellaneous power status data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSJ: TSS-1R, Alpha, Beta, and FDS1/FDS2 status data (SHSJ) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHSK: TSS-1R, Satellite Thruster Status Data IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHTA: TSS-1R, Gyro and Earth Sensor Temperatures IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHTB: TSS-1R, Satellite temperatures IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SHTC: TSS-1R, Satellite temperatures and pressures (SHTC) IDFS format - G. Oelker (Alenia Spazio S.p.A.)
TSS-1R_M1_SPBA: TSS-1R, Space Beam Data IDFS format - Dr Dave Hardy (GL/PHE)
TSS-1R_M1_SPEA: TSS-1R, Selected Electron Spectra From Spectrometer A IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPEB: TSS-1R, Selected Electron Spectra From Spectrometer B IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPEC: TSS-1R, Electron Spectra From Spectrometer A IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPED: TSS-1R, Electron Spectra From Spectrometer B IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPFA: TSS-1R, ESA A, High Frequency Electron Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPFB: TSS-1R, ESA B, High Frequency Electron Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPHA: TSS-1R, Subcommutated Housekeeping Measureents IDFS format - Dr Dave Hardy (GL/PHE)
TSS-1R_M1_SPHB: TSS-1R, FDR Housekeeping Measurements IDFS format - Dr Dave Hardy (GL/PHE)
TSS-1R_M1_SPHC: TSS-1R, FDR Tape Counters IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPHD: TSS-1R, Space Counter Data IDFS format - Dr Dave Hardy (GL/PHE)
TSS-1R_M1_SPHE: TSS-1R, Uplink Command Echo IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPIA: TSS-1R, Zone Summed Ion Spectra From Spectrometer A IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPIB: TSS-1R, Zone Summed Ion Spectra From Spectrometer B IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPIC: TSS-1R, Selected Ion Spectra From Spectrometer A IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPID: TSS-1R, Selected Ion Spectra From Spectrometer B IDFS format - Capt. Marilyn R. Oberhardt (GL/PHE)
TSS-1R_M1_SPIE: TSS-1R, Ion Spectra From Spectrometer A IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPIF: TSS-1R, Ion Spectra From Spectrometer B IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPLA: TSS-1R, Spectrometer A, Low Frequency Ion Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPLB: TSS-1R, ESA A, Low Frequency Electron Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPLC: TSS-1R, Spectrometer B, Low Frequency Ion Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPLD: TSS-1R, ESA B, Low Frequency Electron Auto-Corellation Spectra IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPMF: TSS-1R, Magnetic Field Data IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPOP: TSS-1R, Orbiter Potential Data IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPSA: TSS-1R, SPACE Status And Flow Monitor Data IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPSB: TSS-1R, DPU and FDR Sense Key Status Data IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPSC: TSS-1R, FDR Tape Status IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_SPSD: TSS-1R, DCORE and SETS Gun Status IDFS format - Dr. Dave Hardy (GL/PHE)
TSS-1R_M1_STAA: TSS-1R, Magnetic Field IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STCA: TSS-1R, Current and Charge Probe, Peak Monitors IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STCB: TSS-1R, Direct Current and Charge Probe Monitors IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STCC: TSS-1R, CCP Status Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STCD: TSS-1R, SETS CCP Monitor Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STDA: TSS-1R, DEP and Timing Information IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STDB: TSS-1R, DEP Operation Timing Information IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STDC: TSS-1R, DEP: CPU, GMT and Multibus Time IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STFA: TSS-1R, SETS FPEG Monitors IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STFB: TSS-1R, FPEG Status Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STMA: TSS-1R, SRPA, SPIB and AMAG Power Status Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STMB: TSS-1R, SETS AMAG And SPIB Monitors IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STSA: TSS-1R, Langmuir Probe IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STSB: TSS-1R, Spherical Retarding Potential Analyzer IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STSC: TSS-1R, SETS SRPA Monitors IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STTA: TSS-1R, TCVM Tether Current Monitor IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STTB: TSS-1R, Tether Voltage Monitor IDFS format - Brian Gilchrist (Unversity of Michigan)
TSS-1R_M1_STTC: TSS-1R, SETS TCVM Monitor Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_STTD: TSS-1R, TCVM Relay Status Data IDFS format - Ivan Linscott (Stanford University)
TSS-1R_M1_TMHA: TSS-1R, Housekeeping Data (TMHA) IDFS format - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TSS-1R_M1_TMHB: TSS-1R, Telecommand Echo And Checksum (TMHB) IDFS format - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TSS-1R_M1_TMMI: TSS-1R, Satellite Inboard Magnetometer Data (TMMI) IDFS format - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TSS-1R_M1_TMMO: TSS-1R, Satellite Outboard Magnetometer Data (TMMO) IDFS format - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TSS-1R_M1_TMTA: TSS-1R, Tether Current (TMTA) IDFS format - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TSS-1R_R0_CAS: CAS (Shuttle Ancillary System) Data Sets Follow:
TSS-1R_R0_DCORE: DCORE (Deployer Core Equipment) Data Sets Follow:
TSS-1R_R0_DPLY: DPLY (Deployer Miscellaneous Housekeeping) Data Sets Follow:
TSS-1R_R0_DRB: DRB (Deployable-Retrievable Boom) Data Sets Follow:
TSS-1R_R0_EMP: EMP (End Mass Payload) Data Sets Follow:
TSS-1R_R0_RETE: RETE ( Research on Electrodynamic Tether Effects) Data Sets Follow:
TSS-1R_R0_ROPE: ROPE (Research on Orbital Plasma Electrodynamics) Data setsfollow - Dr. J. David Winningham (Southwest Research Institute)
TSS-1R_R0_SAHK: SAHK (Spacecraft Housekeeping) Data Sets Follow:
TSS-1R_R0_SCORE: SCORE (Satellite Core Equipment) Data Sets Follow:
TSS-1R_R0_SETS: SETS (Shuttle Electrodynamic Tether System) Data Sets Follow:
TSS-1R_R0_SPREE: SPREE (Shuttle Potential and Return Electron Experiment) Data Sets Follow:
TSS-1R_R0_TEMAG: TEMAG (Magnetic Field Experiment to TSS Mission) Data sets follow: - Dr. Franco Mariani (University of Vergata, Departmento Fisica)
TWINS1_AT_DEF: TWINS1 - Spacecraft Attitude - D. McComas (Southwest Research Institute)
TWINS1_HK_1SEC: TWINS Spacecraft 1 - housekeeping - D. McComas & H. Fahr (SwRI & U. Bonn, respectively.)
TWINS1_L1_IMAGER: TWINS Spacecraft 1 - Neutral-atom Spectrometer Level-1 Magnetospheric Images and Image Movies at Full (9 Energy Steps and 15 minute) Resolution - D. McComas (Southwest Research Institute)
TWINS1_L1_LAD: TWINS Spacecraft 1 - Lyman Alpha Detector Level-1 Geocorona Data - D. McComas & H. Fahr (SwRI & U. Bonn, respectively.)
TWINS1_OR_DEF: TWINS1 - Spacecraft Ephemeris - D. McComas (Southwest Research Institute)
TWINS1_TISTORM_IMAGER: Images of plasma sheet ion temperature during storms calculated from ENA measurements - Amy Keesee (West Virginia University)
TWINS2_AT_DEF: TWINS2 - Spacecraft Attitude - D. McComas (Southwest Research Institute)
TWINS2_HK_1SEC: TWINS Spacecraft 2 - housekeeping - D. McComas & H. Fahr (SwRI & U. Bonn, respectively.)
TWINS2_L1_IMAGER: TWINS Spacecraft 2 - Neutral-atom Spectrometer Level-1 Magnetospheric Images and Image Movies at Full (9 Energy Steps and 15 minute) Resolution - D. McComas (Southwest Research Institute)
TWINS2_L1_LAD: TWINS Spacecraft 2 - Lyman Alpha Detector Level-1 Geocorona Data - D. McComas & H. Fahr (SwRI & U. Bonn, respectively)
TWINS2_OR_DEF: TWINS2 - Spacecraft Ephemeris - D. McComas (Southwest Research Institute)
TWINS2_TISTORM_IMAGER: Images of plasma sheet ion temperature during storms calculated from ENA measurements - Amy Keesee (West Virginia University)
TWINS_M2_ENA: Images of plasma sheet ion temperature during storms calculated from ENA measurements - R. M. Katus (Eastern Michigan University)
ULYSSES_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
ULYSSES_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
URANUS_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
URANUS_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
UY_1MIN_VHM: Ulysses VHM 1 minute. - A. Balogh (Imperial College, London, UK)
UY_1SEC_VHM: Ulysses VHM 1 second. - A. Balogh (Imperial College, London, UK)
UY_ALPHA-DISTRIBUTIONS_SWOOPS: Distribution function of alpha particles - David. J. McComas (Princeton/PPPL)
UY_ALPHA-FIT-PARAMETERS_SWOOPS: Fitting parameters to the distribution function of alphas. - David. J. McComas (Princeton/PPPL)
UY_ALPHA-MOMENTS_SWOOPS: Moments of the distribution function of alpha particles - David. J. McComas (Princeton/PPPL)
UY_COHO1HR_MERGED_MAG_PLASMA: Ulysses merged hourly magnetic field, plasma, proton fluxes, and ephermis data - Dr. A. Balogh (magnetic field), Dr. John L. Phillips (plasma) (Imperial College, London, UK, )
UY_H0_GLG: Ulysses/SWICS full resolution matrix rate data - G. Gloeckler, J. Geiss (Department of Physics, University of Maryland, College Park, Maryland, USA; )
UY_M0_AT1: Ulysses AT Tel 1 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_AT2: Ulysses AT Tel 2 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_BAE: Ulysses BAE 3-22 minute resolution. - D McComas (Southwest Research Institute, USA)
UY_M0_BAI: Ulysses BAI 4-8 minute average. - D McComas (Southwest Research Institute, USA)
UY_M0_GRB: Ulysses GRB 5 minute average. - K Hurley (University of California, Berkeley, USA)
UY_M0_HET: Ulysses HET 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_HFT: Ulysses HFT 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_KET: Ulysses KET 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_LET: Ulysses LET 10 minute average. - R. McKibben (University of New Hampshire, USA)
UY_M0_PFRA: Ulysses PFRA 10 minute average data. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_PFRP: Ulysses PFRP 10 minute peak data. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_R144: Ulysses R144 144 second resolution. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_RARA: Ulysses RARA 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_RARP: Ulysses RARP 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_WFBA: Ulysses WFBA 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_WFBP: Ulysses WFBP 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_WFEA: Ulysses WFEA 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M0_WFEP: Ulysses WFEP 10 minute average. - R MacDowall (NASA Goddard Spaceflight Center)
UY_M1_BAI: Ulysses BAI 1 hour average. - D McComas (Southwest Research Institute, USA)
UY_M1_EPA: Ulysses EPAC 1 hour average. - E Keppler (Max Planck Institut fur Aeronomie, )
UY_M1_LF15: Ulysses LF15 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_LF60: Ulysses LF60 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_LM12: Ulysses LM12 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_LM30: Ulysses LM30 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_LMDE: Ulysses LMDE 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_SCS: Ulysses SWI 3.5 hour average. - J Geiss, G Gloeckler (International Space Science Institute, )
UY_M1_SWI: Ulysses SWI 3.5 hour average. - J Geiss, G Gloeckler (International Space Science Institute, )
UY_M1_VHM: Ulysses VHM 1 hour average. - A. Balogh (Imperial College, London, UK)
UY_M1_WART: Ulysses WART 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_M1_WRTD: Ulysses WRTD 1 hour average. - L. Lanzerotti (Bell Laboratories, USA)
UY_PROTON-DISTRIBUTIONS_SWOOPS: Distribution function of protons - David. J. McComas (Princeton/PPPL)
UY_PROTON-FIT-PARAMETERS_SWOOPS: Fitting parameters of the distribution function of protons. - David. J. McComas (Princeton/PPPL)
UY_PROTON-MOMENTS_SWOOPS: Moments of the distribution function of protons - David. J. McComas (Princeton/PPPL)
VENUS_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
VENUS_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
VG1_PWS_LR: Lowrate Plasma Waves Instrument - William Kurth (University of Iowa)
VG1_PWS_WF: Voyager 1, Plasma Waves Science, Wideband Electric Waveforms - W. Kurth (University Iowa)
VG2_PWS_LR: Lowrate Plasma Waves Instrument - William Kurth (University of Iowa)
VG2_PWS_WF: Voyager 2, Plasma Waves Science, Wideband Electric Waveforms - W. Kurth (University Iowa)
VOYAGER-1_LECP_ELEC-BGND-COR-1D: Voyager 1 LECP Background-corrected electron differential fluxes - Rob Decker (The John Hopkins Applied Physics Laboratory)
VOYAGER-1_LECP_LEV-1-RATES: Voyager I LECP Ion-Electron count rates and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-1_LECP_LEV-2-DAILY-AVG: Voyager I LECP Ion-Electron daily averaged fluxes and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-1_LECP_LEV-2-HOURLY-AVG: Voyager I LECP Ion-Electron hourly averaged fluxes and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-1_LECP_LEV-2-SCAN-AVG: Voyager I LECP Ion-Electron scan averaged rates and fluxes with associated uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-2_LECP_ELEC-BGND-COR-1D: voyager 2 LECP Background-corrected electron differential fluxes - Rob Decker (The John Hopkins Applied Physics Laboratory)
VOYAGER-2_LECP_LEV-1-RATES: Voyager II LECP Ion-Electron count rates and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-2_LECP_LEV-2-DAILY-AVG: Voyager II LECP Ion-Electron daily averaged fluxes and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-2_LECP_LEV-2-HOURLY-AVG: Voyager II LECP Ion-Electron hourly averaged fluxes and uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER-2_LECP_LEV-2-SCAN-AVG: Voyager II LECP Ion-Electron scan averaged rates and fluxes with associated uncertainties. - STAMATIOS M KRIMIGIS (The John Hopkins Applied Physics Laboratory)
VOYAGER1_10S_MAG: 9.6 Second Averaged Interplanetary Magnetic Field - Norman F. Ness (Bartol Research Institute)
VOYAGER1_1HR_MAG: hourly average interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER1_2S_MAG: 1.92 Second Averaged Interplanetary Magnetic Field - Norman F. Ness (Bartol Research Institute)
VOYAGER1_48S_MAG: 48 second interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER1_48S_MAG-VIM: Voyager1 Magnetic field VIM - Adam Szabo (NASA GSFC)
VOYAGER1_COHO1HR_MERGED_MAG_PLASMA: Merged hourly magnetic field, plasma, proton fluxes, and ephemeris data - Adam Szabo (NASA GSFC)
VOYAGER1_CRS_DAILY_FLUX: Voyager-1 CRS Daily Averaged Flux - E. C. Stone (California Institute of Technology)
VOYAGER1_PLS_COMPOSITION: Voyager1, VIPER-Fit Plasma Ion Composition near Jupiter - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER1_PLS_ELECTRONS_E1: Voyager-1 Jupiter Low-Energy Electron Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER1_PLS_ELECTRONS_E2: Voyager-1 Jupiter Low-Energy Electron Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER1_PLS_HIRES_PLASMA_DATA: HiRes plasma data - John D. Richardson (Kavli Institute for Astrophysics and Space Research, Massachusetts Institute of Technology.)
VOYAGER1_PLS_IONS_L: Voyager-1 Jupiter Low-Resolution Ion Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER1_PLS_IONS_M: Voyager-1 Jupiter Low-Resolution Ion Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER2_10S_MAG: 9.6 second interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER2_1HR_MAG: hourly average interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER2_2S_MAG: 9.6 second interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER2_48S_MAG: 48 second interplanetary magnetic field - Norman F. Ness (Bartol Research Institute)
VOYAGER2_48S_MAG-VIM: Voyager2 Magnetic field VIM - Adam Szabo (NASA GSFC)
VOYAGER2_COHO1HR_MERGED_MAG_PLASMA: Voyager-2 merged hourly magnetic field, plasma, proton fluxes, and ephemeris data - N. Ness (MAG) and J. Richardson (PLS) (Bartol, MIT)
VOYAGER2_PLS_COMPOSITION: Voyager1, VIPER-Fit Plasma Ion Composition near Jupiter - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER2_PLS_ELECTRONS_E1: Voyager-1 Jupiter Low-Energy Electron Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER2_PLS_ELECTRONS_E2: Voyager-1 Jupiter Low-Energy Electron Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER2_PLS_HIRES_PLASMA_DATA: HiRes plasma data - John D. Richardson (Kavli Institute for Astrophysics and Space Research, Massachusetts Institute of Technology.)
VOYAGER2_PLS_HIRES_PLASMA_DATA_HSH: Voyager 2 high resolution plasma data in the heliosheath - John D. Richardson (Kavli Institute for Astrophysics and Space Research, Massachusetts Institute of Technology)
VOYAGER2_PLS_IONS_L: Voyager-1 Jupiter Low-Resolution Ion Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
VOYAGER2_PLS_IONS_M: Voyager-1 Jupiter Low-Resolution Ion Current Spectra - Dr. John D. Richardson (MIT Kavli Institute)
WILD2_HELIO1DAY_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
WILD2_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
WIND_3DP_ECHSFITS_E0-YR: Wind spacecraft, 3DP accurate electron parameters - Chadi S. Salem (University of California, Berkeley)
WIND_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)
WIND_WAVES_QTNFIT: WIND Radio/Plasma Wave, (WAVES) Quasi-Thermal Noise Key Parameters - Keith Goetz (University of Minnesota)
WIND_WAVES_QTNFIT-FILTERED: WIND Radio/Plasma Wave, (WAVES) Filtered Quasi-Thermal Noise Key Parameters - Keith Goetz (University of Minnesota)
WI_AT_DEF: Wind Definitive Attitude
WI_AT_PRE: Wind Predicted Attitude
WI_EHPD_3DP: Electron energy-angle distributions 100 eV - 30 keV, often at 24 sec, EESA High, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_EHSP_3DP: Electron omnidirectional fluxes 100 eV-30 keV, often at 24 sec, EESA High, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_ELM2_3DP: Electron Moments (ground-computed), EESA Low, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_ELPD_3DP: Electron energy-angle distributions 5-1100 eV, often at 24 sec, EESA Low, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_ELSP_3DP: Electron omnidirectional fluxes 5-1100 eV, often at 24 sec, EESA Low, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_EMFITS_E0_3DP: Wind spacecraft, 3DP electron moments - Stuart D. Bale (University of California, Berkeley)
WI_EM_3DP: Electron Plasma moments (computed on-board) (NOT CORRECTED FOR S/C POTENTIAL) @ 3 second (spin) resolution (version 3), EESA LOW, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_EPACT_STEP-DIFFERENTIAL-ION-FLUX-1HR: Wind EPACT-STEP - Mihir Desai (University of Texas, San Antonio)
WI_EPACT_STEP-DIRECTIONAL-DIFF-CNO-FLUX-10MIN: Wind EPACT-STEP CNO - Mihir Desai (University of Texas, San Antonio)
WI_EPACT_STEP-DIRECTIONAL-DIFF-FE-FLUX-10MIN: Wind EPACT-STEP FE - Mihir Desai (University of Texas, San Antonio)
WI_EPACT_STEP-DIRECTIONAL-DIFF-H-FLUX-10MIN: Wind EPACT-STEP H - Mihir Desai (University of Texas, San Antonio)
WI_EPACT_STEP-DIRECTIONAL-DIFF-HE-FLUX-10MIN: Wind EPACT-STEP HE - Mihir Desai (University of Texas, San Antonio)
WI_H0_MFI: Wind Magnetic Fields Investigation: 3 sec, 1 min, and hourly Definitive Data. - A. Koval (UMBC, NASA/GSFC)
WI_H0_SWE: Wind SOLAR WIND EXPERIMENT 6 - 12 sec solar wind electron moments - K. Ogilvie (GSFC Code 692)
WI_H0_WAV: WIND Radio/Plasma Wave, (WAVES) Key Parameters - M. L. Kaiser (GSFC)
WI_H1_SWE: Solar wind proton and alpha parameters, including anisotropic temperatures, derived by non-linear fitting of the measurements and with moment techniques. - Keith W. Ogilvie (NASA GSFC)
WI_H1_SWE_RTN: Solar wind proton and alpha parameters, including anisotropic temperatures, derived by non-linear fitting of the measurements and with moment techniques. Data in RTN - Bennett Maruca (University of Delaware)
WI_H1_WAV: Wind Radio/Plasma Wave, (WAVES) Hi-Res Parameters - M. L. Kaiser (GSFC)
WI_H2_MFI: Wind Magnetic Fields Investigation, High-resolution Definitive Data - A. Koval (UMBC, NASA/GSFC)
WI_H3-RTN_MFI: Wind Magnetic Fields Investigation: 3 sec, 1 min, and hourly Definitive Data (RTN). - A. Koval (UMBC, NASA/GSFC)
WI_H3_SWE: Wind SOLAR WIND EXPERIMENT 9 sec solar wind electron pitch-angle distributions - K. Ogilvie (NASA/GSFC)
WI_H4-RTN_MFI: Wind Magnetic Fields Investigation, High-resolution Definitive Data (RTN) - A. Koval (UMBC, NASA/GSFC)
WI_H4_SWE: 3 sec solar wind electron pitch-angle distributions at 6-12 sec cadence, Wind Solar Wind Experiment (SWE) - K. Ogilvie (NASA/GSFC)
WI_H5_SWE: Wind SOLAR WIND EXPERIMENT 9 sec solar wind electron moments - K. Ogilvie (NASA/GSFC)
WI_K0_3DP: Wind 3-D Plasma Analyzer, Key Parameters [PRELIM] - R. Lin/S. Bale (UC Berkeley)
WI_K0_EPA: Wind Energetic Particle Acceleration Composition Transport, Key Parameters [PRELIM] - T. Von Roseavinge (NASA/GSFC)
WI_K0_GIFWALK: Links to Wind KP pre-generated survey and other plots - Polar-Wind-Geotail Ground System (NASA GSFC)
WI_K0_MFI: Wind Magnetic Fields Investigation, Key Parameters - R. Lepping (NASA/GSFC)
WI_K0_SMS: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - G. Gloeckler (U of MD Maryland)
WI_K0_SPHA: Wind Spin Phase
WI_K0_SWE: Wind Solar Wind Experiment, Key Parameters - K. Ogilvie (NASA GSFC)
WI_K0_SWE_RTN: Wind Solar Wind Experiment, Key Parameters in RTN - Bennett Maruca (University of Delaware)
WI_K0_WAV: WIND Radio/Plasma Wave, (WAVES) Key Parameters - M. L. Kaiser (GSFC)
WI_K1-RTN_MFI: Wind Magnetic Fields Investigation, Key Parameters in RTN - Andriy Koval (UMBC)
WI_L2-1HOUR-SEP_EPACT-APE_B: Wind EPACT-APE_B H 18.90 -21.90 MeV Solar Energetic Particle Intensities, 1-Hour Level 2 Data - T. Von Rosenvinge & D. Reames (NASA GSFC)
WI_L2-1HOUR-SEP_EPACT-LEMT: Wind EPACT-LEMT He/C/O/Ne/Si/Fe 2-11 MeV/Nuc Solar Energetic Particle Intensities, 1-Hour Level 2 Data - T. Von Rosenvinge & D. Reames (NASA GSFC)
WI_L2-30MIN_SMS-STICS-AFM-MAGNETOSPHERE: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-30MIN_SMS-STICS-AFM-SOLARWIND: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-30MIN_SMS-STICS-ERPA-MAGNETOSPHERE: Magnetosphere and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-30MIN_SMS-STICS-ERPA-SOLARWIND: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-3MIN_SMS-STICS-VDF-MAGNETOSPHERE: Magnetosphere and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-3MIN_SMS-STICS-VDF-SOLARWIND: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2-5MIN-SEP_EPACT-LEMT: Wind EPACT-LEMT He/C/O/Ne/Si/Fe 2-11 MeV/Nuc Solar Energetic Particle Intensities, 5min Level 2 Data - T. Von Rosenvinge & D. Reames (NASA GSFC)
WI_L2_3MIN_SMS-STICS-NVT-MAGNETOSPHERE: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2_3MIN_SMS-STICS-NVT-SOLARWIND: Solar Wind and Suprathermal Ion Composition Instrument, Key Parameters - S. T. Lepri (U of Michigan)
WI_L2_WAV_RAD1: Wind/WAVES/RAD1 Data - Karine Issautier (Karine.Issautier@obspm.fr) (LESIA, Observatoire de Paris-PSL, CNRS)
WI_L2_WAV_RAD2: Wind/WAVES/RAD2 Data - Karine Issautier (Karine.Issautier@obspm.fr) (LESIA, Observatoire de Paris-PSL, CNRS)
WI_L3-DUSTIMPACT_WAVES: The Radio and Plasma Wave Investigation on the Wind Spacecraft - D.M. Malaspina (U. Colorado at Boulder, LASP)
WI_M0_SWE: Wind SOLAR WIND EXPERIMENT 9 sec solar wind electron pitch-angle distribution averages - K. Ogilvie (NASA/GSFC)
WI_M2_SWE: Wind SOLAR WIND EXPERIMENT 3 sec solar wind electron pitch-angle distribution averages - K. Ogilvie (NASA/GSFC)
WI_OR_DEF: Wind Definitive Orbit
WI_OR_GIFWALK: Links to Wind and multi-mission orbit plots - Polar-Wind-Geotail Ground System (NASA GSFC)
WI_OR_PRE: Wind Predicted Orbit
WI_PLSP_3DP: Ion omnidirectional fluxes 0.4-3 keV and moments, often at ~24 second resolution, PESA Low, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_PM_3DP: Ion moments (computed on-board) @ 3 second (spin) resolution, PESA LOW, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_SFPD_3DP: Electron energy-angle distributions 27 keV to 520 keV, often at 24 sec, SST Foil, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_SFSP_3DP: Electron omnidirectional fluxes 27 keV - 520 keV, often at 24 sec, SST Foil, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_SOPD_3DP: Proton energy-angle distributions 70 keV - 6.8 MeV, often at 24 sec, SST Open, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_SOSP_3DP: Proton omnidirectional fluxes 70 keV - 6.8 MeV, often at 24 sec, SST Open, Wind 3DP - R. Lin/S. Bale (UC Berkeley)
WI_STRAHL0_SWE: Wind Solar Wind Experiment (SWE) strahl detector, ~1/2 sec solar wind electron pitch-angle distributions at ~12 sec cadence - K. Ogilvie (NASA/GSFC)
WI_SW-ION-DIST_SWE-FARADAY: Faraday Cup orientation and charge flux - Keith Ogilvie (NASA GSFC)
WI_WA_RAD1_L3_DF: Wind Waves, Level 3 Direction-Finding (DF) parameters - K. Issautier (LESIA, Observatoire de Paris-PSL, CNRS)

A1_K0_MPA doi:10.48322/6jar-ra45
Description
This file contains numerical moments computed from measurements of the 
Los Alamos Magnetospheric Plasma Analyzer (MPA) [Bame et al., 
Rev. Sci. Inst., in press 1993]. 
The moments are presented in s/c coordinates: the z-axis is aligned with 
the spin axis, which points radially toward the center of the Earth; 
the x-axis is in the plane containing the spacecraft spin axis and the spin 
axis of the Earth, with +X generally northward; and the y-axis points 
generally eastward. Polar angles are measured relative to the spin axis 
(+Z), and azimuthal angles are measured around the z-axis, with zero along 
the +X direction. The moments are computed for three 'species': 
lop (low-ener. ions, ~1eV/e-~130eV/e); hip (hi-ener. ions, ~130eV/e-~45keV/e);
 alle (electrons, ~30eV - ~45keV ). The electron measurements are obtained 
21.5 secs after the ion measurements. Epoch is the measurement time 
appropriate for the ions. The moments are computed after the fluxes are 
corrected for background and s/c potential. Algorithms for these corrections
 are relatively unsophisticated, so the moments are suspect during times of 
high background and/or high spacecraft potential. Because the determined  
spacecraft potential is not very precise, the magnitude of the low-energy 
ion flow velocity is probably not accurate, but the flow direction is well 
determined.  Tperp and Tpara are obtained from diagonalization of the  
3-dimensional temperature matrix, with the parallel direction assigned 
to the eigenvalue which is most different from the other two. 
The corresponding eigenvector is the symmetry axis of the distribution and 
should be equivalent to the magnetic field direction. The eigenvalue ratio 
Tperp/Tmid, which is provided for each species, is a measure of the symmetry 
of the distribution and should be ~1.0 for a good determination. Several of  
the parameters have a fairly high daily dynamic range and for survey purposes 
are best displayed logarithmically. These parameters are indicated by  
non-zero 'SCALEMIN' values in this file. A quality flag value of 1  
indicates that the values are suspect because of unreliable 
location info. 
Modification History
Created SEP 1992 Modified JAN 1993 
Electron time tags removed Mag Latitude added 
Local time added Post Gap flag added 
Ratio variables changed Modified SEP 1994 
Changes noted in mail message from M.Kessel 
New Dict keys added sep95 
Added new global attr. and variables from M.Kessel Oct 98
 
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A2_K0_MPA doi:10.48322/z6y7-r007
Description
This file contains numerical moments computed from measurements of the 
Los Alamos Magnetospheric Plasma Analyzer (MPA) [Bame et al., 
Rev. Sci. Inst., in press 1993]. 
The moments are presented in s/c coordinates: the z-axis is aligned with 
the spin axis, which points radially toward the center of the Earth; 
the x-axis is in the plane containing the spacecraft spin axis and the spin 
axis of the Earth, with +X generally northward; and the y-axis points 
generally eastward. Polar angles are measured relative to the spin axis 
(+Z), and azimuthal angles are measured around the z-axis, with zero along 
the +X direction. The moments are computed for three 'species': 
lop (low-ener. ions, ~1eV/e-~130eV/e); hip (hi-ener. ions, ~130eV/e-~45keV/e);
 alle (electrons, ~30eV - ~45keV ). The electron measurements are obtained 
21.5 secs after the ion measurements. Epoch is the measurement time 
appropriate for the ions. The moments are computed after the fluxes are 
corrected for background and s/c potential. Algorithms for these corrections
 are relatively unsophisticated, so the moments are suspect during times of 
high background and/or high spacecraft potential. Because the determined  
spacecraft potential is not very precise, the magnitude of the low-energy 
ion flow velocity is probably not accurate, but the flow direction is well 
determined.  Tperp and Tpara are obtained from diagonalization of the  
3-dimensional temperature matrix, with the parallel direction assigned 
to the eigenvalue which is most different from the other two. 
The corresponding eigenvector is the symmetry axis of the distribution and 
should be equivalent to the magnetic field direction. The eigenvalue ratio 
Tperp/Tmid, which is provided for each species, is a measure of the symmetry 
of the distribution and should be ~1.0 for a good determination. Several of  
the parameters have a fairly high daily dynamic range and for survey purposes 
are best displayed logarithmically. These parameters are indicated by  
non-zero 'SCALEMIN' values in this file. A quality flag value of 1  
indicates that the values are suspect because of unreliable 
location info. 
Modification History
Created SEP 1992 Modified JAN 1993 
Electron time tags removed Mag Latitude added 
Local time added Post Gap flag added 
Ratio variables changed Modified SEP 1994 
Changes noted in mail message from M.Kessel 
New Dict keys added sep95 
Added new global attr. and variables from M.Kessel Oct 98
 
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AC_AT_DEF doi:10.48322/f2a8-nm36
Description
ACE attitude direction cosines (hourly values) in GSE and J2000 GCI coordinate
systems
Modification History
Initial Release 09/20/2012 
 
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AC_H0_MFI doi:10.48322/e0dc-0h53
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/ 
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 9/7/01 
12/04/02: Fixed description of Epoch time variable.
 
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AC_H0_SWE doi:10.48322/tsfn-6v47
Description
SWEPAM - Solar Wind Electron Proton Alpha Monitor 
References: http://www.srl.caltech.edu/ACE/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 02/23/00.
12/04/02: Fixed alpha/proton ratio precision bug.
12/04/02: Fixed description of Epoch time variable.
 
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AC_H1_EPM doi:10.48322/w4wv-rj18
Description
The Electron, Proton, and Alpha Monitor (EPAM) is composed of five 
telescope apertures of three different types.  Two Low Energy 
Foil Spectrometers (LEFS) measure the flux and direction of electrons 
above 30 keV (geometry factor = 0.397 cm2*sr), two Low Energy Magnetic 
Spectrometers (LEMS) measure the flux  and direction of ions greater than 50 keV
(geometry factor = 0.48 cm2*sr), and the Composition Aperture (CA) 
measures the elemental composition of the ions (geometry factor = 0.24 
cm2*sr). The telescopes use the spin of the spacecraft to sweep the full 
sky. Solid-state detectors are used to measure the energy and composition 
of the incoming particles. 
For more information about the EPAM instrument, visit the EPAM Home Page 
at JHU/APL: http://sd-www.jhuapl.edu/ACE/EPAM/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Public Release 01/28/03 (Version 3)
11/11/04: Improved metadata (Version 4) 
 
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AC_H1_MFI doi:10.48322/brf1-g493
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/ 
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 9/6/01 
12/04/02: Fixed description of Epoch time variable.
 
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AC_H1_SIS doi:10.48322/9kmb-8280
Description
The Solar Isotope Spectrometer (SIS) is designed to provide high resolution
measurements of the isotopic composition of 
energetic nuclei from He to Ni (Z=2 to 28) over the energy range from ~10 to
~100 MeV/nucleon. During large  
solar events, when particle fluxes can increase over quiet-time values by
factors of up to 10000, SIS measures the isotopic 
composition of the solar corona, while during solar quiet times SIS measures the
isotopes of low-energy Galactic cosmic rays 
and the composition of the anomalous cosmic rays which are thought to originate
in the nearby interstellar medium.  
The solar energetic particle measurements are useful to further our
understanding of the Sun, while also providing a 
baseline for comparison with the Galactic cosmic ray measurements carried out by
CRIS.  SIS has a geometry factor of ~40 
cm2--sr, which is significantly larger than previous satellite solar particle
isotope spectrometers. It is also 
designed to provide excellent mass resolution during the extremely high particle
flux conditions which occur during 
large solar particle events.
Modification History
Initial Release 02/08/05 
 
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AC_H2_CRIS doi:10.48322/g72t-0814
Description
The Cosmic Ray Isotope Spectrometer (CRIS) on the Advanced Composition
Explorer(ACE) spacecraft is intended to be a major step in ascertaining the
isotopic composition of 
the Galactic Cosmic Rays(GCRs) and hence a major step in determining their
origin. The GCRs consist, by number, primarily of hydrogen nuclei(~92%) and
helium nuclei (~7%). The energetic nuclei from He to Ni (Z=2 to 28) over the
energy range from ~10 to ~100 MeV/nucleon. During large  
solar events, when particle fluxes can increase over quiet-time values by
factors of up to 10000, CRIS measures the isotopic 
composition of the solar corona, while during solar quiet times CRIS measures
the isotopes of low-energy Galactic cosmic rays 
and the composition of the anomalous cosmic rays which are thought to originate
in the nearby interstellar medium.  
The solar energetic particle measurements are useful to further our
understanding of the Sun, while also providing a 
baseline for comparison with the Galactic cosmic ray measurements carried out by
CRIS.  CRIS has a geometry factor of ~40 
cm2--sr, which is significantly larger than previous satellite solar particle
isotope spectrometers. It is also 
designed to provide excellent mass resolution during the extremely high particle
flux conditions which occur during 
large solar particle events.
Modification History
Initial Release 02/08/05 
 
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AC_H2_EPM doi:10.48322/pn1t-zx03
Description
The Electron, Proton, and Alpha Monitor (EPAM) is composed of five 
telescope apertures of three different types.  Two Low Energy 
Foil Spectrometers (LEFS) measure the flux and direction of electrons 
above 30 keV (geometry factor = 0.397 cm2*sr), two Low Energy Magnetic 
Spectrometers (LEMS) measure the flux  and direction of ions greater than 50 keV
(geometry factor = 0.48 cm2*sr), and the Composition Aperture (CA) 
measures the elemental composition of the ions (geometry factor = 0.24 
cm2*sr). The telescopes use the spin of the spacecraft to sweep the full 
sky. Solid-state detectors are used to measure the energy and composition 
of the incoming particles. 
For more information about the EPAM instrument, visit the EPAM Home Page 
at JHU/APL: http://sd-www.jhuapl.edu/ACE/EPAM/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Public Release 01/28/03 (Version 3)
11/11/04: Improved metadata (Version 4) 
 
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AC_H2_MFI doi:10.48322/fh85-fj47
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/ 
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 9/6/01 
12/04/02: Fixed description of Epoch time variable.
 
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AC_H2_SEP doi:10.48322/3086-yq22
Description
The SEPICA Instrument on ACE   
The Solar Energetic Particle Ionic Charge Analyzer 
is the sensor on ACE, which is used to determine the 
charge state distribution of energetic particle distributions.
SEPICA is designed to measure the ionic charge state, Q, 
the kinetic energy, E, and the nuclear charge, Z, of energetic ions above 0.2
MeV/Nuc. 
This includes ions accelerated in solar flares as well as in  
interplanetary space during energetic storm particle (ESP) 
and co-rotating interaction region (CIR) events. For low mass numbers 
SEPICA also separates isotopes -- for example, 3He and 4He. 
For more information about the SEPICA instrument, visit the SEPICA Home Page 
at University of New Hampshire:
http://www.ssg.sr.unh.edu/tof/Missions/Ace/index.html?sepicamain.html 
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 07/27/07 
 
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AC_H2_SIS doi:10.48322/eq1k-gs80
Description
The Solar Isotope Spectrometer (SIS) is designed to provide high resolution
measurements of the isotopic composition of 
energetic nuclei from He to Ni (Z=2 to 28) over the energy range from ~10 to
~100 MeV/nucleon. During large  
solar events, when particle fluxes can increase over quiet-time values by
factors of up to 10000, SIS measures the isotopic 
composition of the solar corona, while during solar quiet times SIS measures the
isotopes of low-energy Galactic cosmic rays 
and the composition of the anomalous cosmic rays which are thought to originate
in the nearby interstellar medium.  
The solar energetic particle measurements are useful to further our
understanding of the Sun, while also providing a 
baseline for comparison with the Galactic cosmic ray measurements carried out by
CRIS.  SIS has a geometry factor of ~40 
cm2--sr, which is significantly larger than previous satellite solar particle
isotope spectrometers. It is also 
designed to provide excellent mass resolution during the extremely high particle
flux conditions which occur during 
large solar particle events.
Modification History
Initial Release 02/08/05 
 
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AC_H2_SWE doi:10.48322/9w01-2555
Description
SWEPAM - Solar Wind Electron Proton Alpha Monitor 
References: http://www.srl.caltech.edu/ACE/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 04/04/02.
12/04/02: Fixed alpha/proton ratio precision bug.
12/04/02: Fixed description of Epoch time variable.
12/04/02: -9999.9 fill-data values changed to -1.0e+31.
 
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AC_H2_SWI doi:10.48322/p7gt-yh33
Description
SWICS 1.1 - The Solar Wind Ion Composition Spectrometer prior to August 23 2011
- 
determines uniquely the chemical and ionic-charge composition of the solar wind,
the temperatures and mean speeds of major solar wind ions, at all speeds 
above 300 km/s (protons) and 170 km/s  (Fe+16), and resolves H and He isotopes 
of solar and interstellar sources. SWICS 1.1 measures the distribution functions
of the interstellar cloud and dust cloud pickup ions up to energies of 100
keV/e.
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 11/08/05 
 
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AC_H2_ULE doi:10.48322/agmq-ex61
Description
The ULEIS Instrument on ACE   
The Ultra Low Energy Isotope Spectrometer 
measures ion fluxes over the charge range from H through Ni from about 
20 keV/nucleon to 10 MeV/nucleon, thus covering both suprathermal and 
energetic particle energy ranges. Exploratory measurements of 
ultra-heavy species (mass range above Ni) will also be performed in a more 
limited energy range near 0.5 MeV/nucleon. 
ULEIS will be studying the elemental and isotopic 
composition of solar energetic particles, and the mechanisms by 
which these particles are energized in the solar corona. ULEIS will 
also investigate mechanisms by which supersonic interplanetary shock 
waves energize ions.
For more information about the ULEIS instrument, visit the ULEIS Home Page 
at JHU/APL: http://sd-www.jhuapl.edu/ACE/ULEIS/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 07/19/04 
 
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AC_H3_CRIS doi:10.48322/wbmv-4z80
Description
The Cosmic Ray Isotope Spectrometer (CRIS) on the Advanced Composition
Explorer(ACE) spacecraft is intended to be a major step in ascertaining the
isotopic composition of 
the Galactic Cosmic Rays(GCRs) and hence a major step in determining their
origin. The GCRs consist, by number, primarily of hydrogen nuclei(~92%) and
helium nuclei (~7%). The energetic nuclei from He to Ni (Z=2 to 28) over the
energy range from ~10 to ~100 MeV/nucleon. During large  
solar events, when particle fluxes can increase over quiet-time values by
factors of up to 10000, CRIS measures the isotopic 
composition of the solar corona, while during solar quiet times CRIS measures
the isotopes of low-energy Galactic cosmic rays 
and the composition of the anomalous cosmic rays which are thought to originate
in the nearby interstellar medium.  
The solar energetic particle measurements are useful to further our
understanding of the Sun, while also providing a 
baseline for comparison with the Galactic cosmic ray measurements carried out by
CRIS.  CRIS has a geometry factor of ~40 
cm2--sr, which is significantly larger than previous satellite solar particle
isotope spectrometers. It is also 
designed to provide excellent mass resolution during the extremely high particle
flux conditions which occur during 
large solar particle events.
Modification History
Initial Release 02/08/05 
 
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AC_H3_EPM doi:10.48322/jqj0-vn49
Description
The Electron, Proton, and Alpha Monitor (EPAM) is composed of five 
telescope apertures of three different types.  Two Low Energy 
Foil Spectrometers (LEFS) measure the flux and direction of electrons 
above 30 keV (geometry factor = 0.397 cm2*sr), two Low Energy Magnetic 
Spectrometers (LEMS) measure the flux  and direction of ions greater than 50 keV
(geometry factor = 0.48 cm2*sr), and the Composition Aperture (CA) 
measures the elemental composition of the ions (geometry factor = 0.24 
cm2*sr). The telescopes use the spin of the spacecraft to sweep the full 
sky. Solid-state detectors are used to measure the energy and composition 
of the incoming particles. 
For more information about the EPAM instrument, visit the EPAM Home Page 
at JHU/APL: http://sd-www.jhuapl.edu/ACE/EPAM/  
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Public Release 01/28/03 (Version 3)
11/11/04: Improved metadata (Version 4) 
 
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AC_H3_MFI doi:10.48322/7xyh-4z44
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/ 
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 03/10/2010 
 
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AC_H3_SW2 doi:10.48322/xcsn-8w62
Description
SWICS 2.0 is The Solar Wind Ion Composition Spectrometer after August 23 2011 
when a radiation and age-induced hardware anomaly altered the instrument's 
operational state. It should not be confused with SWICS 1.1, the recalibrated 
data set extending from launch up to the anomaly. 
SWICS 2.0 determines uniquely the chemical and ionic-charge composition of the
solar wind, 
and the mean speed of solar wind He ions. 
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 11/08/05 
 
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AC_H3_SWI doi:10.48322/mvcn-0276
Description
SWICS 1.1 - The Solar Wind Ion Composition Spectrometer prior to August 23 2011
- 
determines uniquely the chemical and ionic-charge composition of the solar wind,
the temperatures and mean speeds of major solar wind ions, at all speeds 
above 300 km/s (protons) and 170 km/s  (Fe+16), and resolves H and He isotopes 
of solar and interstellar sources. SWICS 1.1 measures the distribution functions
of the interstellar cloud and dust cloud pickup ions up to energies of 100
keV/e.
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 11/08/05 
 
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AC_H4_SWI doi:10.48322/vpnc-ym91
Description
SWICS 1.1 - The Solar Wind Ion Composition Spectrometer prior to August 23 2011 
determines uniquely the chemical and ionic-charge composition of the solar wind,
the temperatures and mean speeds of major solar wind ions, at all speeds 
above 300 km/s (protons) and 170 km/s  (Fe+16), and resolves H and He isotopes 
of solar and interstellar sources. SWICS 1.1 measures the distribution functions
of the interstellar cloud and dust cloud pickup ions up to energies of 100
keV/e.
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 11/08/05 
 
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AC_H5_SWI doi:10.48322/2c38-0s43
Description
SWICS 1.1 - The Solar Wind Ion Composition Spectrometer prior to August 23 2011 
determines uniquely the chemical and ionic-charge composition of the solar wind,
the temperatures and mean speeds of major solar wind ions, at all speeds 
above 300 km/s (protons) and 170 km/s  (Fe+16), and resolves H and He isotopes 
of solar and interstellar sources. SWICS measures the distribution functions
of the interstellar cloud and dust cloud pickup ions up to energies of 100
keV/e.
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 10/10/2012 
 
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AC_H6_SWI doi:10.48322/mfxn-cw77
Description
SWICS - The Solar Wind Ion Composition Spectrometer 
determines uniquely the chemical and ionic-charge composition of the solar wind,
the temperatures and mean speeds of major solar wind ions, at all speeds 
above 300 km/s (protons) and 170 km/s  (Fe+16), and resolves H and He isotopes 
of solar and interstellar sources. SWICS measures the distribution functions 
of the interstellar cloud and dust cloud pickup ions up to energies of 100
keV/e.
For more information about the SWICS instrument, visit the SWICS Home Page at 
http://solar-heliospheric.engin.umich.edu/ace.
The quality of ACE level 2 data is such that it is suitable for serious 
scientific study.  However, to avoid confusion and misunderstanding, it 
is recommended that users consult with the appropriate ACE team members
before publishing work derived from the data. The ACE team has worked 
hard to ensure that the level 2 data are free from errors, but the team 
cannot accept responsibility for erroneous data, or for misunderstandings 
about how the data may be used. This is especially true if the appropriate 
ACE team members are not consulted before publication. At the very 
least, preprints should be forwarded to the ACE team before publication.
Modification History
Initial Release 01/25/17 
 
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AC_K0_EPM doi:10.48322/ghbm-qj24
Description
EPAM - ACE Electron, Proton, and Alpha Monitor
References: http://www.srl.caltech.edu/ACE/ 
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
EPAM Browse data is not validated by the experimenters and should not 
be used except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 04/30/99 
 
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AC_K0_GIFWALK
Description
Pre-generated PWG plots
 
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AC_K0_MFI doi:10.48322/cs7n-7c62
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/  
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
MAG Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 11/10/98 
 
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AC_K0_SIS doi:10.48322/1fgf-zm82
Description
SIS - ACE Solar Isotope Spectrometer
References: http://www.srl.caltech.edu/ACE/ 
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
SIS Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 04/10/99 
 
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AC_K0_SWE doi:10.48322/pfr6-fg57
Description
SWEPAM - Solar Wind Electron Proton Alpha Monitor 
References: http://www.srl.caltech.edu/ACE/ 
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
SWEPAM Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 12/01/98 
 
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AC_K1_EPM doi:10.48322/qgh8-2q85
Description
EPAM - ACE Electron, Proton, and Alpha Monitor
References: http://www.srl.caltech.edu/ACE/ 
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
EPAM Browse data is not validated by the experimenters and should not 
be used except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 08/26/99 
 
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AC_K1_MFI doi:10.48322/av87-m833
Description
MAG - ACE Magnetic Field Experiment
References: http:// www.srl.caltech.edu/ACE/  
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
MAG Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 11/10/98 
 
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AC_K1_SWE doi:10.48322/0n2v-es49
Description
SWEPAM - Solar Wind Electron Proton Alpha Monitor 
References: http://www.srl.caltech.edu/ACE/ 
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
SWEPAM Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 12/01/98 
 
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AC_K2_MFI doi:10.48322/pf44-ys65
Description
MAG - ACE Magnetic Field Experiment
References: http://www.srl.caltech.edu/ACE/  
ACE browse data is designed for monitoring large scale particle and field 
behavior and for selecting interesting time periods. The data is automatically 
generated from the spacecraft data stream using simple algorithms provided by 
the instrument teams. It is not routinely checked for accuracy and is subject 
to revision. Use this data at your own risk, and consult with the appropriate 
instrument teams about citing it. 
MAG Browse data is not validated by the experimenters and should not be used 
except for preliminary examination prior to detailed studies. 
Modification History
Initial Release 11/10/98 
 
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AC_OR_DEF doi:10.48322/mh1w-x115
Description
ACE orbit data (daily values) in GSE and J2000 GCI coordinate systems
Modification History
Initial Release 09/20/2012 
 
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AC_OR_SSC doi:10.48322/by5e-zs07
Description
GROUP 1    Satellite   Resolution   Factor
            ace           720         1
Coord/            Min/Max   Range Filter       Filter
Component   Output Markers  Minimum  Maximum   Mins/Maxes 
GSE X        YES      -        -        -           -        -           -   
GSE Y        YES      -        -        -           -        -           -   
GSE Z        YES      -        -        -           -        -           -   
GSE Lat      YES      -        -        -           -        -           -   
GSE Lon      YES      -        -        -           -        -           -   
Addtnl             Min/Max   Range Filter       Filter
Options     Output Markers  Minimum  Maximum   Mins/Maxes
dEarth       YES      -        -        -           -   
Formats and units:                          
    Day/Time format: YYYY DDD HH:MM
    Degrees/Hemisphere format: Decimal degrees with 2 place(s).
        Longitude 0 to 360, latitude -90 to 90.
    Distance format: Kilometers with 2 place(s).
Modification History
Originated 03/14/96
 
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AEROCUBE-6-A_DOSIMETER_L2 doi:10.48322/gn8x-mj75
Description
Each AeroCube-6 vechicle carries three dosimeters measuring electrons with
energies from about 43 keV to about 830 keV and protons with enegies ranging
from 370 keV to 12 MeV. The dataset manager, Dr. Paul O'Brien, can be reached at
paul.obrien@aero.org. The data are described in AeroCube-6 Dosimeter Data README
(v3.0), Aerospace Report No. TOR-2016-01155, The Aerospace Corporation, March 4,
2016, El Segundo, CA. Also see AeroCube-6 Dosimeter Equivalent Energy Thresholds
and Flux Conversion Factors, Aerospace Report No. TOR-2017-02598, The Aerospace
Corporation, July 1, 2019, El Segundo, CA.
Modification History
N/A
 
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AEROCUBE-6-B_DOSIMETER_L2 doi:10.48322/49dd-na02
Description
Each AeroCube-6 vechicle carries three dosimeters measuring electrons with
energies from about 43 keV to about 830 keV and protons with enegies ranging
from 370 keV to 12 MeV. The dataset manager, Dr. Paul O'Brien, can be reached at
paul.obrien@aero.org. The data are described in AeroCube-6 Dosimeter Data README
(v3.0), Aerospace Report No. TOR-2016-01155, The Aerospace Corporation, March 4,
2016, El Segundo, CA. Also see AeroCube-6 Dosimeter Equivalent Energy Thresholds
and Flux Conversion Factors, Aerospace Report No. TOR-2017-02598, The Aerospace
Corporation, July 1, 2019, El Segundo, CA.
Modification History
N/A
 
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AIM_CIPS_SCI_3A
Description
Aeronomy of Ice in the Mesosphere (AIM),  Cloud Imaging and Particle Size (CIPS)
Polar Mesospheric Clouds (PMC) Albedo images.
There are 15 orbits per day and the data are gridded to form the Level 3A images
 
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ALOUETTE2_AV_LIM doi:10.48322/bq14-8619
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_AV_QUI doi:10.48322/5aep-ew77
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_AV_SNT doi:10.48322/bxt1-c896
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_AV_SOL doi:10.48322/29p2-h053
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_AV_ULA doi:10.48322/kvy0-3088
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_AV_WNK doi:10.48322/nhht-4411
Description
This ionogram was digitized from the original Alouette 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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ALOUETTE2_NEPROF_TOPS (spase://NASA/NumericalData/Alouette2/SFS/PT32S)
Description
This data file contains topside electron density profiles as deduced from
Alouette 2 topside sounder measurements. The data processing was done in the
seventies at the Communications Research Center in Ottawa, Canada This data set
provides data from 1000km down in steps of irregular step size. The x- and
o-traces were manually  scaled from the ionograms and the inversion algorithm of
J. Jackson was used to compute the density profiles from these traces.
 
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AMPTECCE_H0_MEPA doi:10.48322/zz7m-pv06
Description
This dataset contains high time resolution MEPA rate channel data. MEPA is a
particle telescope with an ION head and a TOF head. The TOF head can measure
species and energy, while the ION head only measures the energy of the ions,
which are mostly protons. In fact, the counts in the ION head are all assumed to
be protons up to 1830 keV. The ION head has 10 energy channels, and so the first
8 channels (that are all below 1830 keV) are assumed to be all protons, and the
2 channels above this are assumed to be all alphas. The TOF head has 9 energy
channels that are generic (ions of any species are counted) and some species
specific channels for protons, helium, oxygen, and iron. The AMPTE data was
divided into records, with each record holding data from 4 spins. In any record,
all the TOF species channels are always present, but only one of either a) the
10 ION head channels or b) 9 TOF generic channels are present. The majority of
records have the ION head channels. The AMPTE spacecraft had a spin period of
about 6 seconds. The exact spin period varies slightly and is included in the
data. MEPA data is sectored into 32 directions per spin. Nearly all channels are
reported as sectored values, but to conserve telemetry, many channels are only
read out every other spin, or every fourth spin. In this data, all values are
summed so that they are reported every fourth spin. Note that in the original
AMPTE datesets, there was a timing problem which required that 19.75 seconds
(one Major Frame of telemetry) be added to time values extracted from the
processing system. This correction has already been made in the particle data in
this dataset.
 
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APOLLO12_SWS_1HR doi:10.48322/vars-pj10
Description
This is the hourly-averaged data from the Apollo 12 Solar Wind  Spectrometer 
instrument, reformatted by NSSDC for easier access and use.  During the lunar
night there is no solar wind signal so there are data gaps of about 15 days
each lunation. 
Users should refer to the data set documentation paper entitled 'ALSEP solar
wind spectrometer plasma data as observed at the Apollo 12 and 15 landing
sites,' by Goldstein, Clay,Snyder, and Neugebauer, which is contained in the
online Data Set Catalog at
https://nssdc.gsfc.nasa.gov/nmc/publicationDisplay.do?id=B55381-000A
 
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APOLLO12_SWS_28S doi:10.48322/wh21-c403
Description
This 28-s data set is the highest resolution data set available from the 
Apollo 12 Solar Wind Spectrometer instrument, and was reformatted by NSSDC for
 easier access and use.  During the lunar night there is no solar wind signal
so there are data gaps of about 15 days each lunation.
Users should refer to the data set documentation paper entitled 'ALSEP solar
wind spectrometer plasma data as observed at the Apollo 12 and 15 landing
sites,' by Goldstein, Clay,Snyder, and Neugebauer, which is contained in the
online Data Set Catalog at
https://nssdc.gsfc.nasa.gov/nmc/publicationDisplay.do?id=B55381-000A
 
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APOLLO15_SWS_1HR doi:10.48322/70qp-jj13
Description
This is the hourly-averaged data from the Apollo 15 Solar Wind Spectrometer 
instrument, reformatted by NSSDC for easier access and use.  During the lunar
night there is no solar wind signal so there are data gaps of about 15 days
each lunation.
Users should refer to the data set documentation paper entitled 'ALSEP solar
wind spectrometer plasma data as observed at the Apollo 12 and 15 landing
sites,' by Goldstein, Clay,Snyder, and Neugebauer, which is contained in the
online Data Set Catalog at
https://nssdc.gsfc.nasa.gov/nmc/publicationDisplay.do?id=B55381-000A
 
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APOLLO15_SWS_28S doi:10.48322/97e0-5h57
Description
This 28-s data set is the highest resolution data set available from the 
Apollo 15 Solar Wind Spectrometer instrument, and was reformatted by NSSDC 
for easier access and use.  During the local lunar night there is no solar
wind signal so there are data gaps of about 15 days each lunation.
Users should refer to the data set documentation paper entitled 'ALSEP solar
wind spectrometer plasma data as observed at the Apollo 12 and 15 landing
sites,' by Goldstein, Clay,Snyder, and Neugebauer, which is contained in the
online Data Set Catalog at
https://nssdc.gsfc.nasa.gov/nmc/publicationDisplay.do?id=B55381-000A
 
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AWE_L3A_TMP
Description
AWE investigates the connection between tropospheric weather and space weather -
Visit 'https://www.awemission.org' for more details 
 
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AWE_L3C_Q20
Description
AWE investigates the connection between tropospheric weather and space weather -
Visit 'https://www.awemission.org' for more details 
 
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BAR_1A_L2_EPHM doi:10.48322/6z4h-nc30
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1A_L2_FSPC doi:10.48322/y0xa-nh97
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1A_L2_HKPG doi:10.48322/c6ne-ba73
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1A_L2_MAGN doi:10.48322/w6hk-sg12
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1A_L2_MSPC doi:10.48322/b3tb-2j68
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1A_L2_RCNT doi:10.48322/cs79-7n39
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1A_L2_SSPC doi:10.48322/zf2e-8t15
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1B_L2_EPHM doi:10.48322/6psd-w950
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1B_L2_FSPC doi:10.48322/zwpb-gd36
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1B_L2_HKPG doi:10.48322/jnz6-mm05
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1B_L2_MAGN doi:10.48322/dvz5-6463
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1B_L2_MSPC doi:10.48322/xsac-gy90
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1B_L2_RCNT doi:10.48322/dafb-ne70
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1B_L2_SSPC doi:10.48322/m40j-ew70
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1C_L2_EPHM doi:10.48322/drbp-w973
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1C_L2_FSPC doi:10.48322/gxys-hr97
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1C_L2_HKPG doi:10.48322/48e3-bc29
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1C_L2_MAGN doi:10.48322/8k18-dm67
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1C_L2_MSPC doi:10.48322/hxs2-n143
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1C_L2_RCNT doi:10.48322/m51j-4083
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1C_L2_SSPC doi:10.48322/zejc-sv71
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1D_L2_EPHM doi:10.48322/25t8-6425
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1D_L2_FSPC doi:10.48322/b6ef-hd09
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1D_L2_HKPG doi:10.48322/5zsp-3s97
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1D_L2_MAGN doi:10.48322/jv0x-j569
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1D_L2_MSPC doi:10.48322/64ww-2n81
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1D_L2_RCNT doi:10.48322/4h81-bk40
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1D_L2_SSPC doi:10.48322/4p83-ym30
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1G_L2_EPHM doi:10.48322/h9ph-1g74
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1G_L2_FSPC doi:10.48322/wvky-v338
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1G_L2_HKPG doi:10.48322/axks-mn61
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1G_L2_MAGN doi:10.48322/hgv2-8860
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1G_L2_MSPC doi:10.48322/baq8-f915
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1G_L2_RCNT doi:10.48322/6cs7-wh14
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1G_L2_SSPC doi:10.48322/thhq-y177
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1H_L2_EPHM doi:10.48322/pkpa-h637
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1H_L2_FSPC doi:10.48322/ajq0-7695
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1H_L2_HKPG doi:10.48322/s49a-y430
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1H_L2_MAGN doi:10.48322/by86-xd44
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1H_L2_MSPC doi:10.48322/26s4-6e86
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1H_L2_RCNT doi:10.48322/n4kz-3e94
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1H_L2_SSPC doi:10.48322/g5sq-zk30
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1I_L2_EPHM doi:10.48322/5y5j-a444
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1I_L2_FSPC doi:10.48322/b3my-e903
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1I_L2_HKPG doi:10.48322/w183-cr37
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1I_L2_MAGN doi:10.48322/26k0-7g17
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1I_L2_MSPC doi:10.48322/854v-rh42
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1I_L2_RCNT doi:10.48322/npka-5c76
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1I_L2_SSPC doi:10.48322/rnmb-rf14
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1J_L2_EPHM doi:10.48322/cy7m-z194
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1J_L2_FSPC doi:10.48322/v2p2-dg83
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1J_L2_HKPG doi:10.48322/4pm9-wh04
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1J_L2_MAGN doi:10.48322/ym6r-0a10
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1J_L2_MSPC doi:10.48322/rnt4-0620
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1J_L2_RCNT doi:10.48322/f1rv-gm55
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1J_L2_SSPC doi:10.48322/pnc0-t138
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1K_L2_EPHM doi:10.48322/vx0e-1e48
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1K_L2_FSPC doi:10.48322/syxw-pc22
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1K_L2_HKPG doi:10.48322/a81f-0j09
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
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BAR_1K_L2_MAGN doi:10.48322/thmx-6507
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_1K_L2_MSPC doi:10.48322/zeqt-yf54
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1K_L2_RCNT doi:10.48322/5w2z-j063
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1K_L2_SSPC doi:10.48322/vgdv-8673
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1M_L2_EPHM doi:10.48322/mkdz-qy48
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_1M_L2_FSPC doi:10.48322/wkna-7f79
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_1M_L2_HKPG doi:10.48322/jvbc-xw61
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
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BAR_1M_L2_MAGN doi:10.48322/f4ga-sc28
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
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BAR_1M_L2_MSPC doi:10.48322/syaa-pp39
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_1M_L2_RCNT doi:10.48322/dvng-1e34
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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BAR_1M_L2_SSPC doi:10.48322/np9s-6d14
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_1N_L2_EPHM doi:10.48322/27q1-4486
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
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BAR_1N_L2_FSPC doi:10.48322/vaed-8q27
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1N_L2_HKPG doi:10.48322/667v-0f59
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_1N_L2_MAGN doi:10.48322/p356-6j08
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1N_L2_MSPC doi:10.48322/3th0-gz04
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1N_L2_RCNT doi:10.48322/ntk5-gx95
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1N_L2_SSPC doi:10.48322/jysk-p094
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_EPHM doi:10.48322/h7g5-qk94
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_FSPC doi:10.48322/t156-7k66
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_HKPG doi:10.48322/pjg0-gg59
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_MAGN doi:10.48322/6nf2-qd32
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_MSPC doi:10.48322/cpje-0a97
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_RCNT doi:10.48322/vnnj-3z47
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1O_L2_SSPC doi:10.48322/ksyp-7m93
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_EPHM doi:10.48322/h8fk-8v43
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_FSPC doi:10.48322/9e32-1f82
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_HKPG doi:10.48322/y9yd-dm68
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_MAGN doi:10.48322/fxmc-pd46
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_MSPC doi:10.48322/fpq5-v930
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_RCNT doi:10.48322/kzg3-3n69
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1Q_L2_SSPC doi:10.48322/dv3a-9472
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_EPHM doi:10.48322/wwk9-ag68
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_FSPC doi:10.48322/vb76-v853
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_HKPG doi:10.48322/5xzc-3891
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_MAGN doi:10.48322/4mcm-d772
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_MSPC doi:10.48322/44q9-sk93
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_RCNT doi:10.48322/kga8-wm09
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1R_L2_SSPC doi:10.48322/qnm3-9849
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_EPHM doi:10.48322/stcw-qq17
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_FSPC doi:10.48322/7ww4-qj81
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_HKPG doi:10.48322/tcz9-xv08
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_MAGN doi:10.48322/e5za-b739
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_MSPC doi:10.48322/vfpb-r487
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_RCNT doi:10.48322/sqsh-9282
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1S_L2_SSPC doi:10.48322/25ff-2051
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_EPHM doi:10.48322/qhdw-8857
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_FSPC doi:10.48322/dxv1-1175
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_HKPG doi:10.48322/mz5s-dx74
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_MAGN doi:10.48322/03qh-gb67
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_MSPC doi:10.48322/9tdc-za92
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_RCNT doi:10.48322/x1fx-bj09
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1T_L2_SSPC doi:10.48322/4mqp-9x78
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_EPHM doi:10.48322/5p7b-bk28
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_FSPC doi:10.48322/qvw8-sc52
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_HKPG doi:10.48322/vc63-yg58
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_MAGN doi:10.48322/90zk-0t28
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_MSPC doi:10.48322/317w-4n52
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_RCNT doi:10.48322/mhwm-nd09
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1U_L2_SSPC doi:10.48322/2jk7-k570
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_EPHM doi:10.48322/69e2-g517
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_FSPC doi:10.48322/ajdw-de45
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_HKPG doi:10.48322/fbx5-6364
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_MAGN doi:10.48322/vmhk-5j19
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_MSPC doi:10.48322/kfdn-jm13
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_RCNT doi:10.48322/vyew-jx42
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_1V_L2_SSPC doi:10.48322/hmhs-rj73
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_EPHM doi:10.48322/k17v-zh58
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_FSPC doi:10.48322/m57x-a377
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_HKPG doi:10.48322/ks5e-x703
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_MAGN doi:10.48322/yk33-2j45
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_MSPC doi:10.48322/haak-6g59
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_RCNT doi:10.48322/s6ye-gg42
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2A_L2_SSPC doi:10.48322/zrb7-eh51
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_EPHM doi:10.48322/3cb8-6c41
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_FSPC doi:10.48322/2htf-ef08
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_HKPG doi:10.48322/srkd-2n33
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_MAGN doi:10.48322/4d0f-ke54
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_MSPC doi:10.48322/szae-fh60
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_RCNT doi:10.48322/sdf6-qg21
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2B_L2_SSPC doi:10.48322/7rwb-b613
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_EPHM doi:10.48322/vg72-ck78
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_FSPC doi:10.48322/33vt-pk86
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_HKPG doi:10.48322/w6a4-bh10
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_MAGN doi:10.48322/q5wa-bc13
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_MSPC doi:10.48322/zn2s-8628
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_RCNT doi:10.48322/5c4n-sk89
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2C_L2_SSPC doi:10.48322/agfe-2f18
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_EPHM doi:10.48322/pa71-ct06
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_FSPC doi:10.48322/c7sw-vd47
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_HKPG doi:10.48322/9rrg-s874
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_MAGN doi:10.48322/6q2f-2j62
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_MSPC doi:10.48322/26r4-w775
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_RCNT doi:10.48322/j9px-y347
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2D_L2_SSPC doi:10.48322/qpk7-em74
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_EPHM doi:10.48322/gs6h-hk87
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_FSPC doi:10.48322/hcw9-w939
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_HKPG doi:10.48322/fqj7-dv29
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_MAGN doi:10.48322/e3dc-ca32
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_MSPC doi:10.48322/j2ag-a553
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_RCNT doi:10.48322/c0bc-ny12
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2E_L2_SSPC doi:10.48322/acm6-5w68
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_EPHM doi:10.48322/ez86-kg25
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_FSPC doi:10.48322/5b6w-8b58
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_HKPG doi:10.48322/mdk4-s678
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_MAGN doi:10.48322/rsr2-kr32
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_MSPC doi:10.48322/e6ch-hx32
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_RCNT doi:10.48322/gjen-0231
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2F_L2_SSPC doi:10.48322/kgnz-hk70
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_EPHM doi:10.48322/seqv-5070
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_FSPC doi:10.48322/dbkq-7r26
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_HKPG doi:10.48322/ptm1-0195
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_MAGN doi:10.48322/8d6a-ye59
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_MSPC doi:10.48322/zpr6-0t37
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_RCNT doi:10.48322/wk9f-1z22
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2I_L2_SSPC doi:10.48322/e3qj-p998
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_EPHM doi:10.48322/wzv1-4232
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_FSPC doi:10.48322/r87y-ft15
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_HKPG doi:10.48322/xqee-4x09
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_MAGN doi:10.48322/nmph-2c10
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_MSPC doi:10.48322/bpex-1580
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_RCNT doi:10.48322/6chq-a612
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2K_L2_SSPC doi:10.48322/81ce-c654
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_EPHM doi:10.48322/2rp7-fc02
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_FSPC doi:10.48322/3phr-hg17
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_HKPG doi:10.48322/vpmt-pa22
Description
Voltage, temperature, current, and payload status values returned every 40s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_MAGN doi:10.48322/3kam-t980
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_MSPC doi:10.48322/f1p2-en15
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_RCNT doi:10.48322/sd8x-yv62
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a 4 second accumulation.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2L_L2_SSPC doi:10.48322/k96c-em33
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_EPHM doi:10.48322/ve82-v240
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_FSPC doi:10.48322/23ep-4d26
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_HKPG doi:10.48322/cgt7-j364
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_MAGN doi:10.48322/kazt-tk82
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_MSPC doi:10.48322/540t-a510
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_RCNT doi:10.48322/n60z-7r73
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2M_L2_SSPC doi:10.48322/zhdg-4032
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_EPHM doi:10.48322/vcq8-a194
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_FSPC doi:10.48322/0p2y-ge65
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_HKPG doi:10.48322/mer9-cq38
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_MAGN doi:10.48322/g5z3-bg91
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_MSPC doi:10.48322/nnvk-bd41
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_RCNT doi:10.48322/r05q-ne63
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2N_L2_SSPC doi:10.48322/s47j-y384
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_EPHM doi:10.48322/7d2h-d765
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_FSPC doi:10.48322/9dnf-9q17
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_HKPG doi:10.48322/f3a4-kc09
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_MAGN doi:10.48322/hbn0-ed44
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_MSPC doi:10.48322/jqy7-v984
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_RCNT doi:10.48322/wmv8-qy98
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2O_L2_SSPC doi:10.48322/e6v8-mw75
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_EPHM doi:10.48322/rncw-7m94
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_FSPC doi:10.48322/vpq4-qq24
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_HKPG doi:10.48322/cpdt-pn06
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_MAGN doi:10.48322/5bsk-hr87
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_MSPC doi:10.48322/9pn2-q783
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_RCNT doi:10.48322/wcsq-3h51
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2P_L2_SSPC doi:10.48322/wy87-9b67
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_EPHM doi:10.48322/mzbd-3w07
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_FSPC doi:10.48322/bdf5-qy57
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_HKPG doi:10.48322/emkt-d141
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_MAGN doi:10.48322/dy96-b422
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_MSPC doi:10.48322/fhf4-8149
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_RCNT doi:10.48322/vkgs-yb27
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Q_L2_SSPC doi:10.48322/p9y0-9339
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_EPHM doi:10.48322/1dnz-5546
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_FSPC doi:10.48322/362k-9s76
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_HKPG doi:10.48322/hxx4-xw56
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_MAGN doi:10.48322/zyfb-em84
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_MSPC doi:10.48322/7cm2-j892
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_RCNT doi:10.48322/fa3p-vm65
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2T_L2_SSPC doi:10.48322/mep9-ew14
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_EPHM doi:10.48322/686v-cj69
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_FSPC doi:10.48322/2qs7-6888
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_HKPG doi:10.48322/8yxs-k148
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_MAGN doi:10.48322/41r3-pk06
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_MSPC doi:10.48322/sfr2-c574
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_RCNT doi:10.48322/zk66-9z83
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2W_L2_SSPC doi:10.48322/c2ry-tr16
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_EPHM doi:10.48322/hjr5-e182
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_FSPC doi:10.48322/ravw-5f48
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_HKPG doi:10.48322/b59z-vy34
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_MAGN doi:10.48322/k50e-7b59
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_MSPC doi:10.48322/0884-ya29
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_RCNT doi:10.48322/2hyd-p019
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2X_L2_SSPC doi:10.48322/1rzk-fj72
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_EPHM doi:10.48322/6ct2-7m72
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_FSPC doi:10.48322/gfv6-mp73
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_HKPG doi:10.48322/q3gf-7k21
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_MAGN doi:10.48322/58mf-ha76
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_MSPC doi:10.48322/qskf-jg98
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_RCNT doi:10.48322/9s7d-md89
Description
Rate counters record interrupt, low level, peak detect, and high level. Each
value is a four second accumulation
 
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Data Access Code Examples written in Python and IDL®.
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BAR_2Y_L2_SSPC doi:10.48322/br21-hq14
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_EPHM doi:10.48322/rf94-w711
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_FSPC doi:10.48322/ndyh-wr73
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_HKPG doi:10.48322/jag5-cj38
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_MAGN doi:10.48322/vx93-wa27
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_MSPC doi:10.48322/qaax-ap13
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_RCNT doi:10.48322/gf3k-qk78
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3A_L2_SSPC doi:10.48322/y2av-tc84
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_EPHM doi:10.48322/xg1n-0b95
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_FSPC doi:10.48322/zfva-7247
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_HKPG doi:10.48322/5axh-d034
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_MAGN doi:10.48322/vgpv-9j39
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_MSPC doi:10.48322/45b0-zh24
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_RCNT doi:10.48322/crfn-yj32
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3B_L2_SSPC doi:10.48322/9695-st55
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_EPHM doi:10.48322/1fk8-z856
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_FSPC doi:10.48322/kaq2-2n16
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_HKPG doi:10.48322/j6tc-qr91
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_MAGN doi:10.48322/7kzj-8892
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_MSPC doi:10.48322/vmwt-tj82
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_RCNT doi:10.48322/gaq1-e914
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3C_L2_SSPC doi:10.48322/bypk-cz78
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_EPHM doi:10.48322/m49n-7f05
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_FSPC doi:10.48322/4ezv-t009
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_HKPG doi:10.48322/8m2m-a059
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_MAGN doi:10.48322/gtyx-m063
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_MSPC doi:10.48322/11nj-q752
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_RCNT doi:10.48322/dgg1-gn58
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_3D_L2_SSPC doi:10.48322/qrg9-0r11
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_EPHM doi:10.48322/9gcz-1f05
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_FSPC doi:10.48322/ycaj-t234
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_HKPG doi:10.48322/gvhe-3y17
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_MAGN doi:10.48322/qsee-cc93
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_MSPC doi:10.48322/9he8-2n21
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_RCNT doi:10.48322/e8hc-xc72
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3E_L2_SSPC doi:10.48322/3t6h-hq76
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_EPHM doi:10.48322/bnx3-b780
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_FSPC doi:10.48322/evmz-ex46
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_HKPG doi:10.48322/v1w6-nc88
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_MAGN doi:10.48322/5xj6-ja79
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_MSPC doi:10.48322/811n-3b48
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_RCNT doi:10.48322/3sjj-r365
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3F_L2_SSPC doi:10.48322/s4vw-m998
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_EPHM doi:10.48322/n222-b468
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_FSPC doi:10.48322/1fcc-za91
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_HKPG doi:10.48322/8kje-3r88
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_MAGN doi:10.48322/znf7-mh36
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_MSPC doi:10.48322/bm2e-fv03
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_RCNT doi:10.48322/x9pb-4e60
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_3G_L2_SSPC doi:10.48322/rsp5-6d40
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_EPHM doi:10.48322/an8a-3b17
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_FSPC doi:10.48322/7s7b-3229
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_HKPG doi:10.48322/t8gq-8s91
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_MSPC doi:10.48322/3789-pf08
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_RCNT doi:10.48322/s0hp-4t50
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_SSPC doi:10.48322/55np-j827
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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Data Access Code Examples written in Python and IDL®.
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BAR_4A_L2_USPC doi:10.48322/qqaw-g498
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4A_L2_XSPC doi:10.48322/2skp-j632
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_EPHM doi:10.48322/501n-7c49
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_FSPC doi:10.48322/e1nn-pv68
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_HKPG doi:10.48322/72c2-2d03
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_MSPC doi:10.48322/jh4p-wt91
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_RCNT doi:10.48322/egxz-qr75
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_SSPC doi:10.48322/yjge-sb94
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_USPC doi:10.48322/x1vj-7e22
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4B_L2_XSPC doi:10.48322/7f5h-rk69
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_EPHM doi:10.48322/xm4d-w960
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_FSPC doi:10.48322/73vs-tb09
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_HKPG doi:10.48322/7vxz-fd54
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_MSPC doi:10.48322/fadd-w378
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_RCNT doi:10.48322/100t-5m08
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_SSPC doi:10.48322/fhn8-ab85
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_USPC doi:10.48322/0exd-5863
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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BAR_4C_L2_XSPC doi:10.48322/t582-z012
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_4D_L2_EPHM doi:10.48322/e7qc-bf96
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_4D_L2_FSPC doi:10.48322/87qk-y542
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_4D_L2_HKPG doi:10.48322/vw4w-5p31
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_4D_L2_MSPC doi:10.48322/vxa0-6x03
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_4D_L2_RCNT doi:10.48322/81g2-6868
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_4D_L2_SSPC doi:10.48322/2vk5-5621
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_4D_L2_USPC doi:10.48322/te8x-0295
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4D_L2_XSPC doi:10.48322/h5aq-6g83
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_4E_L2_EPHM doi:10.48322/j5ay-np19
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_4E_L2_FSPC doi:10.48322/dcqb-7a76
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_4E_L2_HKPG doi:10.48322/aaft-vd56
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_4E_L2_MSPC doi:10.48322/731v-ey55
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_4E_L2_RCNT doi:10.48322/yedd-xa76
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_4E_L2_SSPC doi:10.48322/3qq3-f376
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_4E_L2_USPC doi:10.48322/3azn-hd29
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4E_L2_XSPC doi:10.48322/zbb6-g597
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_4F_L2_EPHM doi:10.48322/7w8a-8m45
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_4F_L2_FSPC doi:10.48322/mq7h-3g02
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_4F_L2_HKPG doi:10.48322/mfdf-mz87
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_4F_L2_MSPC doi:10.48322/r6db-7n65
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_4F_L2_RCNT doi:10.48322/9g5m-f692
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_4F_L2_SSPC doi:10.48322/akna-3594
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_4F_L2_USPC doi:10.48322/d1b9-1265
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4F_L2_XSPC doi:10.48322/pnpm-1517
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_4G_L2_EPHM doi:10.48322/jnd7-q680
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_4G_L2_FSPC doi:10.48322/n53n-4k42
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_4G_L2_HKPG doi:10.48322/j7v3-sv26
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_4G_L2_MSPC doi:10.48322/vgsj-k850
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_4G_L2_RCNT doi:10.48322/hs03-wp02
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_4G_L2_SSPC doi:10.48322/rdhd-z209
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_4G_L2_USPC doi:10.48322/evdm-e082
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4G_L2_XSPC doi:10.48322/9bjd-aq22
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_4H_L2_EPHM doi:10.48322/es6y-6n86
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_4H_L2_FSPC doi:10.48322/rpat-8t81
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_4H_L2_HKPG doi:10.48322/2891-0775
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_4H_L2_MSPC doi:10.48322/3ndc-mp02
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_4H_L2_RCNT doi:10.48322/j2w5-a591
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_4H_L2_SSPC doi:10.48322/0j1v-3a83
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_4H_L2_USPC doi:10.48322/np9h-zy23
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_4H_L2_XSPC doi:10.48322/h0qm-2s69
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_5A_L2_EPHM doi:10.48322/hj7s-z115
Description
Geographic and magnetic corrdinates. Geographic coordinates are obtained from
onboard GPS unit, magnegic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_5A_L2_FSPC doi:10.48322/1tv8-2n28
Description
Fast time resolution Bremsstrahlung X-ray spectrum from NaI Scintillator, four
channels at 20 MHz.
 
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BAR_5A_L2_HKPG doi:10.48322/9dg9-d695
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_5A_L2_MSPC doi:10.48322/x8y9-f014
Description
Bremsstrahlung X-ray spectra made of 48 transmitted over 4 frames and
accumulated for 4 seconds.
 
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BAR_5A_L2_RCNT doi:10.48322/vn0r-ca50
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_5A_L2_SSPC doi:10.48322/3ea8-3f36
Description
Bremsstrahlung X-ray spectra each made of 256 energy channels transmitted over
32 frames.
 
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BAR_5A_L2_USPC doi:10.48322/q41s-0145
Description
Bremsstrahlung X-ray spectra each made of 30 raw enery channels. Each record is
a 10ms accumulation. The energy levels for bins in each record are tracked in
the 'energy' support data variable. NOTE: Unlike other BARREL products, these
data are not filtered by altitude (i.e. data below 25km are not removed).
Altitude should be checked in the EPHM file for the time period you are
interested in before use.
 
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BAR_5A_L2_XSPC doi:10.48322/8qm4-cx89
Description
Bremsstrahlung X-ray spectra made of 30 standardized bins with each sample
accumulated for 50ms. The energy levels are constant and set in the 'energy'
support data variable. NOTE: Unlike other BARREL products, these data are not
filtered by altitude (i.e. data below 25km are not removed). Altitude should be
checked in the EPHM file for the time period you are interested in before use
 
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BAR_6A_L2_EPHM
Description
Geographic and magnetic coordinates. Geographic coordinates are obtained from an
onboard GPS unit, magnetic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_6A_L2_FSPC
Description
Six channels of fast time resolution (50ms) Bremsstrahlung X-rays detected with
a NaI Scintillator. Each channel is separated in its own variable (e.g. FSPC1,
FSPC2, etc). Nominal energy range covered by the 6 channels is 0 - 1.5MeV.
 
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BAR_6A_L2_HKPG
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_6A_L2_MAGN
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_6A_L2_MSPC
Description
48 channels (0 - 4MeV) of medium time resolution (4s) Bremsstrahlung X-rays
detected with a NaI Scintillator. All channels are combined to a single variable
(MSPC). 
 
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BAR_6A_L2_RCNT
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_6A_L2_SSPC
Description
256 channels (0-10Mev) of slow time resolution (32s) Bremsstrahlung X-rays
detected with a NaI Scintillator. All channels are combined to a single variable
(SSPC).
 
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BAR_7A_L2_EPHM
Description
Geographic and magnetic coordinates. Geographic coordinates are obtained from an
onboard GPS unit, magnetic coordinates are derived using the IRBEM FORTRAN
library. Ephemeris data products (Lat, Long, Alt, and Time) are each returned
from the payload once every 4s.
 
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BAR_7A_L2_FSPC
Description
Six channels of fast time resolution (50ms) Bremsstrahlung X-rays detected with
a NaI Scintillator. Each channel is separated in its own variable (e.g. FSPC1,
FSPC2, etc). Nominal energy range covered by the 6 channels is 0 - 1.5MeV.
 
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BAR_7A_L2_HKPG
Description
Voltage, temperature, current, and payload status values returned every 40s.
NOTE: The analog sensor data in these records are based on the nominal BARREL
housekeeping layout. Some payloads may have small differences that are not
reflected here. If there is specific sensor data that you need, but looks
questionable, contact the BARREL team for clarification.
 
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BAR_7A_L2_MAGN
Description
Three axis magnetometer reading with nominal conversion. Data are neither gain
corrected nor despun.
 
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BAR_7A_L2_MSPC
Description
48 channels (0 - 4MeV) of medium time resolution (4s) Bremsstrahlung X-rays
detected with a NaI Scintillator. All channels are combined to a single variable
(MSPC). 
 
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BAR_7A_L2_RCNT
Description
Rate counters are diagnostic fields, have uncalibrated energy ranges, and wrap
near or above 16384 counts/second. Values are stored as 4 second accumulations
of counts.
 
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BAR_7A_L2_SSPC
Description
256 channels (0-10Mev) of slow time resolution (32s) Bremsstrahlung X-rays
detected with a NaI Scintillator. All channels are combined to a single variable
(SSPC).
 
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BEPICOLOMBO_HELIO1DAY_POSITION doi:10.48322/cyec-7n35
Proper citations should include the "Accessed on date" in the form .
Description
No TEXT global attribute value.
 
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BEPICOLOMBO_HELIO1HR_POSITION doi:10.48322/cyec-7n35
Proper citations should include the "Accessed on date" in the form .
Description
No TEXT global attribute value.
 
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BIOSENTINEL_LET_LETS
Description
NASA's BioSentinel is a 6U CubeSat launched on Artemis I that is studying the
biological effects of the deep space radiation environment. The spacecraft is in
earth-trailing heliocentric orbit and carries a Linear Energy Transfer
Spectrometer LETS to capture energetic particle dose rates.
NASA's first biological study in interplanetary deep space: 
(a) Combines bio studies with autonomous capability & dosimetry beyond Low Earth
Orbit (LEO); 
(b) Beyond the protection of Earth's magnetosphere; 
(c) Compare radiation environments (deep space, LEO, Earth)
 
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BORRELLY_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/Borrelly/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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BORRELLY_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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C1_CP_CIS-CODIF_H1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HE1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_H1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_H1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_HE1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_O1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_HS_O1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_O1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_PAD_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_PAD_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-CODIF_PAD_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-CODIF_CAVEATS
 
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C1_CP_CIS-HIA_HS_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_MAG_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_MAG_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_MAG_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_SW_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_SW_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_HS_SW_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_LS_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_LS_SW_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_LS_SW_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_LS_SW_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_CIS-HIA_PAD_HS_MAG_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C1_CQ_CIS-HIA_CAVEATS
 
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C1_CP_EDI_AEDC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/16 s for normal and 1/128 s for burst mode 
The AEC (*.edi_ae_cor) files were used to correct for angular (theta-phi)
dependence of the efficieny
The correction is applied to the original CDF files delivered by the EDI team
 
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C1_CP_EDI_MP
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Non-regularly spaced time-series! It contains quarter-spin, half-spin
and spin resolution data with all qualities: GOOD/CAUTION/BAD. 
The values 2/1/0 for GOOD/CAUTION/BAD are  written to Status[0].
Data from spin, half spin and quarter spin IFF files are merged by an algorithm
that can be
thought of as a 'use more if not lower quality' algorithm.
The analysis is performed on each spin's worth of data starting
with spin resolution. If there is more data of half spin 
resolution with equal or better quality, it replaces the spin
resolution data. Likewise, if there is more data of quarter 
spin resolution with equal or better quality, it replaces the
half spin resolution data.
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
DATASET VERSION HISTORY
VERSION 01: The first version of this dataset was converted by the CAA
from source CDF files provided by the EDI team. This conversion involved
insertion of a half interval parameter that was not included in the source
files and correction of missing or bad metadata. The half interval
determination was based on comparison with the spin time-tags provided
in the EDI CSDS Prime Parameter data file. In some cases a consistent
determination could not be found with the PP data and the half-interval
was set to the minimum, quarter spin, 1 second, value.
CDF to CEF Conversion was done using revision 1.1 (2006/11/06) of
edi_mp_convert.pro
Metadata correction was done using revision 1.1 (2006/11/06) of edi_fix_fatal.sh
FILE VERSION HISTORY
For this initial conversion the CAA CEF files have retained the same file
version number as the source CDF files. In most cases file versions are
V13 or V14.
VERSION 02: Minor changes
 
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C1_CP_EDI_QZC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/8 s for normal and 1/64 s for burst mode 
MIN_TIME_RESOLUTION is set to fill_value
MAX_TIME_RESOLUTION is given for BM
Not regularly spaced timeline 
The background electron counts at fixed energy and pitch angle may be
contaminated with beam electrons 
Status parameter has two bits for electron energy and acquisition time for the
electron counts
bit0=0: acquisition time=1/512 s; bit0=1: acq_time=1/1024 s 
bit1 is the energy flag=0/1 for 1/0.5 keV electron energy
 
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C1_CP_EDI_SPIN
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Spin resolution data with GOOD/CAUTION qualities.
The values 2/1 for GOOD/CAUTION are in Status[0].
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
 
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C1_CP_EFW_L3_E3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C1_CP_FGM_5VPS
 - CL_SP_AUX
 - C1_CP_AUX_POSGSE_1M
 
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C1_CP_EFW_L3_P
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
Level 3 quantity P is the negative of the spacecraft potential,
calculated by averaging the Level 2 quantity P over 4 seconds.
For more information on data quality and how the CAA data are processed,
please consult the EFW CAA Users Guide and the EFW CAA Interface Control
Document (ICD).
Detailed quality information is provided as a 16 bit set of flags
in the parameter P_bitmask__C1_CP_EFW_L3_P. The meaning of
the bits is as follows (LSB numbering starting at 0):
Bit  0: Reset.
Bit  1: Bad bias.
Bit  2: Probe latchup.
Bit  3: Low density saturation (-68V).
Bits 4-12: N/A
Bit 13: Whisper operating.
Bit 14: Saturation due to high bias current.
Bit 15: N/A
 
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C1_CP_EFW_L3_V3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C1_CP_FGM_5VPS
 - CL_SP_AUX
 - C1_CP_AUX_POSGSE_1M
 
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C1_CP_FGM_5VPS
Description
Each Cluster spacecraft carries an identical FGM instrument
(Fluxgate Magnetometer) to measure the DC magnetic field
vector. Each instrument, in turn, consists of two triaxial
fluxgate magnetometers and an onboard data processing unit.
The instrument samples the magnetic field at a cadence of 22 Hz
(67 Hz in Burst mode). In order to minimise the magnetic 
background of the spacecraft, one of the magnetometer sensors
 (the outboard, or OB sensor) is located at the end of one
 of the two 5 m radial booms of the spacecraft, the other 
(the inboard, or IB sensor) at 1.5 m inboard from the end 
of the boom. Since the start of the scientific operations 
on February 1, 2001, only the outboard sensor on each 
satellite has been used.
Modification History
*C1_CQ_FGM_CAVF
 
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C1_CP_FGM_SPIN (spase://ESA/NumericalData/Cluster-Rumba/FGM/SpinResolution/PT4S)
Description
No TEXT global attribute value.
 
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C1_CP_RAP_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_ESPCT6
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_HSPCT
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_I3DM_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_I3DM_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_I3DM_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_ISPCT_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_ISPCT_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_PAD_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_PAD_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_PAD_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_PAD_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_RAP_PAD_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C1_CQ_RAP_CAVEATS
*C1_CP_RAP_DSETTINGS
 
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C1_CP_STA_CWF_GSE
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C1_CQ_STA_CALIB_YTR_CAVEATS
*C1_CQ_STA_NOTSRP_MTR_CAVEATS
DATASET VERSION HISTORY
Version 01: First version of dataset.
Version 02: Few corrected re-deliveries.
Version 03: Removal of on-board calibration records is now based on
the calibration bit (instead of the step-in-cal character).
 
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C1_CP_STA_PPP
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C1_CQ_STA_SA_UNDEF_MFA_TR_CAVEATS
*C1_CQ_STA_NOTSRP_MTR_CAVEATS
*C1_CQ_STA_CALIB_YTR_CAVEATS
DATASET VERSION HISTORY:
Version 09 : Reprocessed due to FGM and/or SPD-AUX files re-deliveries.
Version 08 : FGM induced gaps revised and completed.
Version 07 : New calibration tables plus addition of the half-interval 
duration and status. Removal of onboard calibration data.
Now with FGM induced gaps. FGM file used described in the FILE_CAVEATS 
metadata section. 
Warning to the users of versions lower than 07:
Delta_plus of Time__C1_CP_STA_PPP variables was set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate).
Note that the data themselves are correct.
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Version 05: used the new calibration tables (feb 2013).
Version 03: AUX files in CDF format used are 26 hours.
Same data than version02 but less missing values.
Version 02: Data format corrected.
Version 01: Obsolete. Should not be used !
 
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C1_CP_STA_PSD
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C1_CQ_STA_SA_PSD_NEG_CAVEATS
*C1_CQ_STA_NOTSRP_MTR_CAVEATS
*C1_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C1_CP_STA_PSD variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the usual minimum time resolution (1s)
which is correct in most of the time (Normal Bit Rate).
The  time resolution is better in High Bit Rate.
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
The PSD negative values in the version 03 have been replaced 
by the fillvalue (-1.00E+31).
Version 03:
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Phase rotation corrected + exhaustive data. Older versions 
are obsolete and should not be used ! The negative values must not be
taken into account by the users.
Version 02 : Obsolete. This version may be used if Version 03 is not 
available, as long as only total B and total E power are used !
Version 01 : Obsolete. Should not be used !
 
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C1_CP_STA_SM
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C1_CQ_STA_NOTSRP_MTR_CAVEATS
*C1_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C1_CP_STA_SM variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate)
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
Units and Si Conversion of the variables BB and BE have been corrected.
Version 03 : Phase rotation corrected + exhaustive data. 
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Older versions are obsolete and should not be used ! 
Version 02 : Obsolete. Should not be used !
Version 01 : Obsolete. Should not be used !
 
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C1_CP_WHI_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C1_CP_WHI_ELECTRON_DENSITY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update, QUALITY changed to CONTRAST, addition of a
new QUALITY variable
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C1_CP_WHI_NATURAL
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C1_CP_WHI_PASSIVE_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C1_CP_WHI_WAVE_FORM_ENERGY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C1_JP_PMP (spase://ESA/NumericalData/Cluster-Rumba/Ephemeris/JP/PredictedMagneticPosition/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation used to calculate magnetic field and L value 
 in PMP files produced after 23 Feb 2020.
Caveats
JSOC predicted magnetic positions.
 
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C1_JP_PSE (spase://ESA/NumericalData/Cluster-Rumba/Ephemeris/JP/PredictedScientificEvent/PT0.016S)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
AP _ Apogee
CY 1 Start of visibility window at Canberra (5 deg elevation)
CY 2 Start of visibility window at Canberra (5 deg elevation)
CY 3 Start of visibility window at Canberra (5 deg elevation)
CZ 1 End of visibility window at Canberra (5 deg elevation)
CZ 2 End of visibility window at Canberra (5 deg elevation)
CZ 3 End of visibility window at Canberra (5 deg elevation)
CZ 4 End of visibility window at Canberra (5 deg elevation)
DY 1 Start of visibility window at Vilspa (5 deg elevation)
DY 2 Start of visibility window at Vilspa (5 deg elevation)
DY 3 Start of visibility window at Vilspa (5 deg elevation)
DY 4 Start of visibility window at Vilspa (5 deg elevation)
DY 5 Start of visibility window at Vilspa (5 deg elevation)
DZ 1 End of visibility window at Vilspa (5 deg elevation)
DZ 2 End of visibility window at Vilspa (5 deg elevation)
DZ 3 End of visibility window at Vilspa (5 deg elevation)
DZ 4 End of visibility window at Vilspa (5 deg elevation)
GY 1 Start of visibility window at Goldstone (5 deg elevation)
GY 2 Start of visibility window at Goldstone (5 deg elevation)
GY 3 Start of visibility window at Goldstone (5 deg elevation)
GY 4 Start of visibility window at Goldstone (5 deg elevation)
GZ 1 End of visibility window at Goldstone (5 deg elevation)
GZ 2 End of visibility window at Goldstone (5 deg elevation)
GZ 3 End of visibility window at Goldstone (5 deg elevation)
JY 1 Start of visibility window at Maspalomas (5 deg elevation)
JY 2 Start of visibility window at Maspalomas (5 deg elevation)
JY 3 Start of visibility window at Maspalomas (5 deg elevation)
JY 4 Start of visibility window at Maspalomas (5 deg elevation)
JZ 1 End of visibility window at Maspalomas (5 deg elevation)
JZ 2 End of visibility window at Maspalomas (5 deg elevation)
JZ 3 End of visibility window at Maspalomas (5 deg elevation)
KA 1 Start of visibility window at Kourou (5 deg elevation)
KA 2 Start of visibility window at Kourou (5 deg elevation)
KA 3 Start of visibility window at Kourou (5 deg elevation)
KA 4 Start of visibility window at Kourou (5 deg elevation)
KL 1 End of visibility window at Kourou (5 deg elevation)
KL 2 End of visibility window at Kourou (5 deg elevation)
KL 3 End of visibility window at Kourou (5 deg elevation)
KL 4 End of visibility window at Kourou (5 deg elevation)
MY 1 Start of visibility window at Madrid (5 deg elevation)
MY 2 Start of visibility window at Madrid (5 deg elevation)
MY 3 Start of visibility window at Madrid (5 deg elevation)
MY 4 Start of visibility window at Madrid (5 deg elevation)
MZ 1 End of visibility window at Madrid (5 deg elevation)
MZ 2 End of visibility window at Madrid (5 deg elevation)
MZ 3 End of visibility window at Madrid (5 deg elevation)
NS S Southbound neutral sheet
NT I Enter north tail lobe from inner magnetosphere
PA 1 Start of visibility window at Perth (5 deg elevation)
PA 2 Start of visibility window at Perth (5 deg elevation)
PA 3 Start of visibility window at Perth (5 deg elevation)
PA 4 Start of visibility window at Perth (5 deg elevation)
PE _ Perigee
PL 1 End of visibility window at Perth (5 deg elevation)
PL 2 End of visibility window at Perth (5 deg elevation)
PL 3 End of visibility window at Perth (5 deg elevation)
PL 4 End of visibility window at Perth (5 deg elevation)
PL 5 End of visibility window at Perth (5 deg elevation)
QL I Inbound critical L value for auroral zone
QL O Outbound critical L value for auroral zone
RA 1 Start of visibility window at Redu (5 deg elevation)
RA 2 Start of visibility window at Redu (5 deg elevation)
RA 3 Start of visibility window at Redu (5 deg elevation)
RA 4 Start of visibility window at Redu (5 deg elevation)
RL 1 End of visibility window at Redu (5 deg elevation)
RL 2 End of visibility window at Redu (5 deg elevation)
RL 3 End of visibility window at Redu (5 deg elevation)
RL 4 End of visibility window at Redu (5 deg elevation)
RL 5 End of visibility window at Redu (5 deg elevation)
ST O Leave south tail lobe for inner magnetosphere
TL I Inbound radiation belt entry for WEC
TL O Outbound radiation belt exit for WEC
VL I Inbound critical L value for EDI
VL O Outbound critical L value for EDI
XL I Inbound critical L value for PEACE
XL O Outbound critical L value for PEACE
YL I Inbound critical L value for RAPID
YL O Outbound critical L value for RAPID
ZL I Inbound critical L value for CIS
ZL O Outbound critical L value for CIS
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate GSM latitude and MLT 
 in PSE files produced after 23 Feb 2020.
PSE files updated to support orbits >999 and six decimal figures 
 on orbit phase from 25 March 2006.
Caveats
JSOC predicted scientific events.
 
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C1_PP_ASP (spase://ESA/NumericalData/Cluster-Rumba/ASPOC/PrimeParameter/PT4S)
Description
K. Torkar et al, Active spacecraft potential control for Cluster -
implementation and first results
Ann. Geophys., 19,  pp 1289 - 1302, 2001)
Modification History
none
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
 
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C1_PP_CIS (spase://ESA/NumericalData/Cluster-Rumba/CIS/PrimeParameter/PT4S)
Description
H. Reme et al, First multispacecraft ion measurements in and near 
the Earth's magnetosphere with the identical 
Cluster Ion Spectrometry (CIS) experiment
Annales Geophysicae, 19, pp 1303 - 1354, 2001
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C1_PP_CIS_20220930 pre-validated by CIS team and supplied to UKCDC for inges
The user of the CIS data needs to be cautious.
Please refer to the CIS Home Page:
http://cluster.irap.omp.eu/index.php?page=caveats ,
link [Caveats for specific data intervals], for caveats concerning these data.
 
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C1_PP_DWP (spase://ESA/NumericalData/Cluster-Rumba/DWP/PrimeParameter/PT4S)
Description
L. J. C. Woolliscroft et al, The Digital Wave-Processing Experiment on Cluster
Space Sci. Rev., 79,  pp 209 - 231, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C1_PP_DWP_20220702 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
This CSDS DWP product has not been validated prior to release.
 
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C1_PP_EDI doi:10.48322/3cp4-n849
Description
G. Paschmann et al, The Electron Drift Instrument for Cluster
Space Sci. Rev., 79,  pp 233 - 269, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
1) EDI's automated analysis algorithm has a known susceptibility to
producing occasional incorrect values of the drift velocities (and electric
fields). The code attempts to prevent these bad values to be output
to the cdf file. No further removal is done in the validation process.
2) When drift velocities become sufficiently large, there can be a
180-degree ambiguity in drift direction that is usually flagged in bit 7
(counting from 0) of Status Byte 3.
3) There are two methods to analyze a spin's worth of EDI data. If bits 5 &
6 in Status Byte 3 are NOT set, the employed method was triangulation. If
either bit 5 or 6 are set, then the results are from time-of-flight
analysis.
4) The reported drift velocities and electric field refer to inertial
coordinates, i.e., have been corrected for spacecraft velocity. However, the
magnitude errors (in %) and the angle errors (in degrees), reported in
Status Bytes 5 & 6, respectively, refer to the spacecraft frame and have NOT
yet been converted to inertial coordinates.
5) The reduced chi-square reported as a data word is a measure of the
goodness-of-fit of the triangulation analysis.
 
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C1_PP_EFW (spase://ESA/NumericalData/Cluster-Rumba/EFW/PrimeParameter/PT4S)
Description
G. Gustafsson et al, The Electric Field and Wave Experiment for Cluster
Space Sci. Rev., 79,  pp 137 - 156, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data calibration may be unreliable at this early stage of the mission
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** CSDS data are not for publication ***
Be aware that data may be reprocessed as necessary to improve quality
For questions on data validity please contact sdc-adm@plasma.kth.se
Fill value inserted for E_dusk__C1_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_pow_f1__C1_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_sigma__C1_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for U_probe_sc__C1_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_dusk__C1_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for E_pow_f1__C1_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for E_sigma__C1_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for U_probe_sc__C1_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
 
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C1_PP_PEA (spase://ESA/NumericalData/Cluster-Rumba/PEACE/PrimeParameter/PT4S)
Description
A. D. Johnstone et al, Peace, A Plasma Electron and Current Experiment
Space Sci. Rev., 79,  pp 351 - 398, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
PP & SP data is generated at MSSL, then provided to UK-CDHF
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
This is PEACE PP/SP data version 3.1, produced at MSSL
Based on onboard moments but using corrected geometric factors which account for
uplinked changes of the values used in onboard calibration as well as estimated
changes due to variable MCP gain performance
Onboard moments are calculated for up to three energy ranges. Photoelectron
contamination may affect 0, 1 or 2 of these ranges
EFW PP probe-spacecraft potential was used to select the energy ranges to be
excluded to remove misleading photoelectron contributions. Note that the density
may be underestimated if there are both plasma electrons and photoelectrons in
the lowest energy range
When 88h58 is used for the HEEA sensor, sometimes the entire plasma electron
population and photoelectrons are in just the lowest of the 3 energy ranges.
This data has been deleted in this release of the PEACE PPs
Data is deleted if the spacecraft electric potential is too large for the simple
correction procedure to work or there is no EFW PP data available
Measured electron energies have not been corrected for their acceleration by the
spacecraft electric potential
Onboard moments use onboard energy tables, efficiencies and response surfaces.
Any errors in these parameters cannot be corrected in ground data processing
Before 2001-09-11 the onboard energy efficiencies were not accurate, which
caused the density in the solar wind to be overestimated. This data has been
removed in this release of the PEACE PPs
The calculation of T_par, T_perp and Q_par used PP FGM data
The data is for context and information only. It is not suitable for detailed
analysis, but may be used for event selection
The next iteration of PP/SP moments will be of a higher quality
Please see links under
http://www.mssl.ucl.ac.uk/www_plasma/missions/cluster/clusterII.html for more
information
Please contact the PEACE PI to request science quality data
Automatically validated by UKCDC
Product delivered pre-validated by the PI institute
 
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C1_PP_RAP (spase://ESA/NumericalData/Cluster-Rumba/RAPID/PrimeParameter/PT4S)
Description
B. Wilken et al, RAPID, The Imaging Energetic Particle Spectrometer on Cluster
Space Sci. Rev., 79,  pp 399 - 473, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data processed on 2024-11-14T07:34:19Z
Caveats file: RAP_CAV_C1_V245.DAT; Release Sep 16, 2024
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
2023-09-19T00:00:00.000Z/9999-12-31T23:59:59.000Z: RAPID permanently turned off
as of Sep 19, 2023.
Corrected time stamps for ions and electrons.
Energy threshold shifts have been applied.
 
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C1_PP_STA (spase://ESA/NumericalData/Cluster-Rumba/STAFF/PrimeParameter/PT4S)
Description
N. Cornilleau et al,
The Cluster Spatio-Temporal Analysis of Field Fluctuations (Staff) Experiment
Space Sci. Rev., 79,  pp 107 - 136, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
PI Software Version 4.2, 25 September 2006
 
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C1_PP_WHI (spase://ESA/NumericalData/Cluster-Rumba/WHISPER/PrimeParameter/PT4S)
Description
P. M. E. Decreau et al, WHISPER, A Resonance Sounder and Wave Analyser:
Performances and Perspectives for the Cluster Mission
Space Sci. Rev., 79,  pp 157 - 193, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Two types of parameters are provided by WHISPER:
1) Density values (and quality): N_e_res and N_e_res_q, are related to sounding
operations.
The N_e_res value is calculated from an algorithm for resonance recognition,
which cannot take account of all level of information available to the
experimenter. The reliability of N_e_res parameters derived at the CSDS level
is thus limited in an unknown manner.
The N_e_res_q parameter (one value for each N_e_res data point) provides a crude
idea of the probability that the N_e_res value is actually correct. A value of
0 means that the value is probably wrong, a value above 80 that it is probably
correct. Anything in between reflects a crude evaluation of the chances. Refer
to PI for details.
2) Wave power values: E_pow_f4, E_pow_f5, E_pow_f6, E_pow_su and E_var_ts, are
related to recording of natural wave emissions.
Those parameters, not affected by variations in instrument's transfer functions,
are globally OK.
However, two factors can affect the precision of the measurements:
a) the occasional presence of spurious emissions created by operations of the
EDI instrument increases the wave power values measured on SC1, SC2 and SC3,
from an unknown amount,
b) the limited dynamical range of the instrument leads to an underestimation of
the E_pow parameters values when the voltage difference measured by the double
sphere antenna signal in the 2 - 80 kHz band is higher than 150 mVp or 600 mVp
(depending of the gain chosen). As a consequence, high values have to be taken
with special caution.
 
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C1_UP_FGM (spase://ESA/NumericalData/Cluster-Rumba/FGM/UnvalidatedParameter/PT4S)
Description
A. Balogh et al, The Cluster Magnetic Field Investigation
Space Sci. Rev., 79,  pp 65 - 92, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C1_UP_FGM_20240930 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
For the extended mission (starting 1/1/2006) CSDS FGM products
are not validated prior to release to the science community.
Spikes and other artefacts that were previously removed during
validation of the FGM PP/SP data may occur in these files.
 
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C1_WAVEFORM_WBD doi:10.48322/7jw6-ks09
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bands in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'cluster_wbd_calibration.pdf'. Because the calibration was applied in the time
domain using a simple equation the raw counts actually measured by the WBD
instrument can be obtained by using these equations and solving for 'Raw
Counts', keeping in mind that this number is an Integer ranging from 0 to 255. 
Since DC offset is a real number, the resultant when solving for raw counts will
need to be converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, the
following steps need to be carried out:  1) If Electric Field, first divide
calibrated data by 1000 to get V m^-1; 2) Apply window of preference, if any
(such as Hanning, etc.); 3) Divide data values by sqrt(2) to get back to the rms
domain; 4) perform FFT (see Bandwidth variable notes for non-continuous modes);
5) divide by the noise bandwidth, which is equal to the sampling frequency
divided by the FFT size (see table below for appropriate sampling frequency); 6)
multiply by the appropriate constant for the window used, if any.
...
Bandwidth   Sample Rate
---------   ------------
9.5 kHz      27.443 kHz 
19 kHz       54.886 kHz 
77 kHz      219.544 kHz 
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Mar 2008.Revised Dec 2008, Jan 2010
 
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C1_WAVEFORM_WBD_BM2 doi:10.48322/pr6f-rd05
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bandwidths in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'CAA_EST_CR_WBD_v20.pdf'. Because the calibration was applied in the time domain
using a simple equation the raw counts actually measured by the WBD instrument
can be obtained by using these equations and solving for 'Raw Counts', keeping
in mind that this number is an Integer ranging from 0 to 255.  Since DC offset
is a real number, the resultant when solving for raw counts will need to be
converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, see
'CAA_EST_CR_WBD_v20.pdf'. The steps for converting are briefly outlined below:
1) If Electric Field, first divide calibrated data by 1000 to get V m^-1; 2)
Apply window of preference, if any (such as Hanning, etc.); 3) Divide data
values by sqrt(2) to get back to the rms domain; 4) perform FFT (see Bandwidth
VAR_NOTES for non-continuous modes); 5) divide by the noise bandwidth, which is
equal to the sampling frequency divided by the FFT size (see table in VAR_NOTES
of the 'BM_Mode' variable for the appropriate sampling frequency); 6) multiply
by the appropriate constant for the window used, if any;7) if Translation is not
equal to 0, add the appropriate translation frequency to each frequency
component (see Translation CATDESC for the exact values).
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Nov 2014.
 
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C2_CP_EDI_AEDC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/16 s for normal and 1/128 s for burst mode 
The AEC (*.edi_ae_cor) files were used to correct for angular (theta-phi)
dependence of the efficieny
The correction is applied to the original CDF files delivered by the EDI team
 
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C2_CP_EDI_MP
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Non-regularly spaced time-series! It contains quarter-spin, half-spin
and spin resolution data with all qualities: GOOD/CAUTION/BAD. 
The values 2/1/0 for GOOD/CAUTION/BAD are  written to Status[0].
Data from spin, half spin and quarter spin IFF files are merged by an algorithm
that can be
thought of as a 'use more if not lower quality' algorithm.
The analysis is performed on each spin's worth of data starting
with spin resolution. If there is more data of half spin 
resolution with equal or better quality, it replaces the spin
resolution data. Likewise, if there is more data of quarter 
spin resolution with equal or better quality, it replaces the
half spin resolution data.
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
DATASET VERSION HISTORY
VERSION 01: The first version of this dataset was converted by the CAA
from source CDF files provided by the EDI team. This conversion involved
insertion of a half interval parameter that was not included in the source
files and correction of missing or bad metadata. The half interval
determination was based on comparison with the spin time-tags provided
in the EDI CSDS Prime Parameter data file. In some cases a consistent
determination could not be found with the PP data and the half-interval
was set to the minimum, quarter spin, 1 second, value.
CDF to CEF Conversion was done using revision 1.1 (2006/11/06) of
edi_mp_convert.pro
Metadata correction was done using revision 1.1 (2006/11/06) of edi_fix_fatal.sh
FILE VERSION HISTORY
For this initial conversion the CAA CEF files have retained the same file
version number as the source CDF files. In most cases file versions are
V13 or V14.
VERSION 02: Minor changes
 
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C2_CP_EDI_QZC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/8 s for normal and 1/64 s for burst mode 
MIN_TIME_RESOLUTION is set to fill_value
MAX_TIME_RESOLUTION is given for BM
Not regularly spaced timeline 
The background electron counts at fixed energy and pitch angle may be
contaminated with beam electrons 
Status parameter has two bits for electron energy and acquisition time for the
electron counts
bit0=0: acquisition time=1/512 s; bit0=1: acq_time=1/1024 s 
bit1 is the energy flag=0/1 for 1/0.5 keV electron energy
 
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C2_CP_EDI_SPIN
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Spin resolution data with GOOD/CAUTION qualities.
The values 2/1 for GOOD/CAUTION are in Status[0].
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
 
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C2_CP_EFW_L3_E3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C2_CP_FGM_5VPS
 - CL_SP_AUX
 - C2_CP_AUX_POSGSE_1M
 
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C2_CP_EFW_L3_P
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
Level 3 quantity P is the negative of the spacecraft potential,
calculated by averaging the Level 2 quantity P over 4 seconds.
For more information on data quality and how the CAA data are processed,
please consult the EFW CAA Users Guide and the EFW CAA Interface Control
Document (ICD).
Detailed quality information is provided as a 16 bit set of flags
in the parameter P_bitmask__C2_CP_EFW_L3_P. The meaning of
the bits is as follows (LSB numbering starting at 0):
Bit  0: Reset.
Bit  1: Bad bias.
Bit  2: Probe latchup.
Bit  3: Low density saturation (-68V).
Bits 4-12: N/A
Bit 13: Whisper operating.
Bit 14: Saturation due to high bias current.
Bit 15: N/A
 
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C2_CP_EFW_L3_V3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C2_CP_FGM_5VPS
 - CL_SP_AUX
 - C2_CP_AUX_POSGSE_1M
 
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C2_CP_FGM_5VPS
Description
Each Cluster spacecraft carries an identical FGM instrument
(Fluxgate Magnetometer) to measure the DC magnetic field
vector. Each instrument, in turn, consists of two triaxial
fluxgate magnetometers and an onboard data processing unit.
The instrument samples the magnetic field at a cadence of 22 Hz
(67 Hz in Burst mode). In order to minimise the magnetic 
background of the spacecraft, one of the magnetometer sensors
 (the outboard, or OB sensor) is located at the end of one
 of the two 5 m radial booms of the spacecraft, the other 
(the inboard, or IB sensor) at 1.5 m inboard from the end 
of the boom. Since the start of the scientific operations 
on February 1, 2001, only the outboard sensor on each 
satellite has been used.
Modification History
*C2_CQ_FGM_CAVF
 
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C2_CP_FGM_SPIN (spase://ESA/NumericalData/Cluster-Salsa/FGM/SpinResolution/PT4S)
Description
No TEXT global attribute value.
 
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C2_CP_RAP_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_ESPCT6
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_HSPCT
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_I3DM_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_I3DM_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_I3DM_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_ISPCT_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_ISPCT_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_PAD_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_PAD_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_PAD_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_RAP_PAD_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C2_CQ_RAP_CAVEATS
*C2_CP_RAP_DSETTINGS
 
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C2_CP_STA_CWF_GSE
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C2_CQ_STA_CALIB_YTR_CAVEATS
*C2_CQ_STA_NOTSRP_MTR_CAVEATS
DATASET VERSION HISTORY
Version 01: First version of dataset.
Version 02: Few corrected re-deliveries.
Version 03: Removal of on-board calibration records is now based on
the calibration bit (instead of the step-in-cal character).
 
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C2_CP_STA_PPP
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C2_CQ_STA_SA_UNDEF_MFA_TR_CAVEATS
*C2_CQ_STA_NOTSRP_MTR_CAVEATS
*C2_CQ_STA_CALIB_YTR_CAVEATS
DATASET VERSION HISTORY:
Version 09 : Reprocessed due to FGM and/or SPD-AUX files re-deliveries.
Version 08 : FGM induced gaps revised and completed.
Version 07 : New calibration tables plus addition of the half-interval 
duration and status. Removal of onboard calibration data.
Now with FGM induced gaps. FGM file used described in the FILE_CAVEATS 
metadata section. 
Warning to the users of versions lower than 07:
Delta_plus of Time__C2_CP_STA_PPP variables was set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate).
Note that the data themselves are correct.
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Version 05: used the new calibration tables (feb 2013).
Version 03: AUX files in CDF format used are 26 hours.
Same data than version02 but less missing values.
Version 02: Data format corrected.
Version 01: Obsolete. Should not be used !
 
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C2_CP_STA_PSD
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C2_CQ_STA_SA_PSD_NEG_CAVEATS
*C2_CQ_STA_NOTSRP_MTR_CAVEATS
*C2_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C2_CP_STA_PSD variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the usual minimum time resolution (1s)
which is correct in most of the time (Normal Bit Rate).
The  time resolution is better in High Bit Rate.
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
The PSD negative values in the version 03 have been replaced 
by the fillvalue (-1.00E+31).
Version 03:
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Phase rotation corrected + exhaustive data. Older versions 
are obsolete and should not be used ! The negative values must not be
taken into account by the users.
Version 02 : Obsolete. This version may be used if Version 03 is not 
available, as long as only total B and total E power are used !
Version 01 : Obsolete. Should not be used !
 
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C2_CP_STA_SM
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C2_CQ_STA_NOTSRP_MTR_CAVEATS
*C2_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C2_CP_STA_SM variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate)
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
Units and Si Conversion of the variables BB and BE have been corrected.
Version 03 : Phase rotation corrected + exhaustive data. 
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Older versions are obsolete and should not be used ! 
Version 02 : Obsolete. Should not be used !
Version 01 : Obsolete. Should not be used !
 
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C2_CP_WHI_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C2_CP_WHI_ELECTRON_DENSITY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update, QUALITY changed to CONTRAST, addition of a
new QUALITY variable
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C2_CP_WHI_NATURAL
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C2_CP_WHI_PASSIVE_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C2_CP_WHI_WAVE_FORM_ENERGY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C2_JP_PMP (spase://ESA/NumericalData/Cluster-Salsa/Ephemeris/JP/PredictedMagneticPosition/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation used to calculate magnetic field and L value 
 in PMP files produced after 23 Feb 2020.
Caveats
JSOC predicted magnetic positions.
 
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C2_JP_PSE (spase://ESA/NumericalData/Cluster-Salsa/Ephemeris/JP/PredictedScientificEvent/PT0.016S)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
AP _ Apogee
CY 1 Start of visibility window at Canberra (5 deg elevation)
CY 2 Start of visibility window at Canberra (5 deg elevation)
CY 3 Start of visibility window at Canberra (5 deg elevation)
CZ 1 End of visibility window at Canberra (5 deg elevation)
CZ 2 End of visibility window at Canberra (5 deg elevation)
CZ 3 End of visibility window at Canberra (5 deg elevation)
CZ 4 End of visibility window at Canberra (5 deg elevation)
DY 1 Start of visibility window at Vilspa (5 deg elevation)
DY 2 Start of visibility window at Vilspa (5 deg elevation)
DY 3 Start of visibility window at Vilspa (5 deg elevation)
DY 4 Start of visibility window at Vilspa (5 deg elevation)
DZ 1 End of visibility window at Vilspa (5 deg elevation)
DZ 2 End of visibility window at Vilspa (5 deg elevation)
DZ 3 End of visibility window at Vilspa (5 deg elevation)
GY 1 Start of visibility window at Goldstone (5 deg elevation)
GY 2 Start of visibility window at Goldstone (5 deg elevation)
GY 3 Start of visibility window at Goldstone (5 deg elevation)
GY 4 Start of visibility window at Goldstone (5 deg elevation)
GZ 1 End of visibility window at Goldstone (5 deg elevation)
GZ 2 End of visibility window at Goldstone (5 deg elevation)
GZ 3 End of visibility window at Goldstone (5 deg elevation)
JY 1 Start of visibility window at Maspalomas (5 deg elevation)
JY 2 Start of visibility window at Maspalomas (5 deg elevation)
JY 3 Start of visibility window at Maspalomas (5 deg elevation)
JY 4 Start of visibility window at Maspalomas (5 deg elevation)
JZ 1 End of visibility window at Maspalomas (5 deg elevation)
JZ 2 End of visibility window at Maspalomas (5 deg elevation)
JZ 3 End of visibility window at Maspalomas (5 deg elevation)
KA 1 Start of visibility window at Kourou (5 deg elevation)
KA 2 Start of visibility window at Kourou (5 deg elevation)
KA 3 Start of visibility window at Kourou (5 deg elevation)
KA 4 Start of visibility window at Kourou (5 deg elevation)
KL 1 End of visibility window at Kourou (5 deg elevation)
KL 2 End of visibility window at Kourou (5 deg elevation)
KL 3 End of visibility window at Kourou (5 deg elevation)
KL 4 End of visibility window at Kourou (5 deg elevation)
MY 1 Start of visibility window at Madrid (5 deg elevation)
MY 2 Start of visibility window at Madrid (5 deg elevation)
MY 3 Start of visibility window at Madrid (5 deg elevation)
MY 4 Start of visibility window at Madrid (5 deg elevation)
MZ 1 End of visibility window at Madrid (5 deg elevation)
MZ 2 End of visibility window at Madrid (5 deg elevation)
MZ 3 End of visibility window at Madrid (5 deg elevation)
NS S Southbound neutral sheet
NT I Enter north tail lobe from inner magnetosphere
PA 1 Start of visibility window at Perth (5 deg elevation)
PA 2 Start of visibility window at Perth (5 deg elevation)
PA 3 Start of visibility window at Perth (5 deg elevation)
PE _ Perigee
PL 1 End of visibility window at Perth (5 deg elevation)
PL 2 End of visibility window at Perth (5 deg elevation)
PL 3 End of visibility window at Perth (5 deg elevation)
PL 4 End of visibility window at Perth (5 deg elevation)
QL I Inbound critical L value for auroral zone
QL O Outbound critical L value for auroral zone
RA 1 Start of visibility window at Redu (5 deg elevation)
RA 2 Start of visibility window at Redu (5 deg elevation)
RA 3 Start of visibility window at Redu (5 deg elevation)
RA 4 Start of visibility window at Redu (5 deg elevation)
RL 1 End of visibility window at Redu (5 deg elevation)
RL 2 End of visibility window at Redu (5 deg elevation)
RL 3 End of visibility window at Redu (5 deg elevation)
RL 4 End of visibility window at Redu (5 deg elevation)
ST O Leave south tail lobe for inner magnetosphere
TL I Inbound radiation belt entry for WEC
TL O Outbound radiation belt exit for WEC
VL I Inbound critical L value for EDI
VL O Outbound critical L value for EDI
WL I Inbound critical L value for ASPOC
WL O Outbound critical L value for ASPOC
XL I Inbound critical L value for PEACE
XL O Outbound critical L value for PEACE
YL I Inbound critical L value for RAPID
YL O Outbound critical L value for RAPID
ZL I Inbound critical L value for CIS
ZL O Outbound critical L value for CIS
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate GSM latitude and MLT 
 in PSE files produced after 23 Feb 2020.
PSE files updated to support orbits >999 and six decimal figures 
 on orbit phase from 25 March 2006.
Caveats
JSOC predicted scientific events.
 
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C2_PP_ASP (spase://ESA/NumericalData/Cluster-Salsa/ASPOC/PrimeParameter/PT4S)
Description
K. Torkar et al, Active spacecraft potential control for Cluster -
implementation and first results
Ann. Geophys., 19,  pp 1289 - 1302, 2001)
Modification History
none
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
One raw data format (5.1.5 secs) of bad data may occur
when the instrument is powered on.
 
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C2_PP_DWP (spase://ESA/NumericalData/Cluster-Salsa/DWP/PrimeParameter/PT4S)
Description
L. J. C. Woolliscroft et al, The Digital Wave-Processing Experiment on Cluster
Space Sci. Rev., 79,  pp 209 - 231, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C2_PP_DWP_20220702 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
This CSDS DWP product has not been validated prior to release.
 
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C2_PP_EDI (spase://NASA/NumericalData/Cluster-Salsa/EDI/PrimeParameter/PT4S)
Description
G. Paschmann et al, The Electron Drift Instrument for Cluster
Space Sci. Rev., 79,  pp 233 - 269, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
The guns are switched off since 2004/04/10 because of strong
interferences with WHISPER. Only Ambient Electron data have been measured
 
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C2_PP_EFW (spase://ESA/NumericalData/Cluster-Salsa/EFW/PrimeParameter/PT4S)
Description
G. Gustafsson et al, The Electric Field and Wave Experiment for Cluster
Space Sci. Rev., 79,  pp 137 - 156, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data calibration may be unreliable at this early stage of the mission
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** CSDS data are not for publication ***
Be aware that data may be reprocessed as necessary to improve quality
For questions on data validity please contact sdc-adm@plasma.kth.se
 
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C2_PP_PEA (spase://ESA/NumericalData/Cluster-Salsa/PEACE/PrimeParameter/PT4S)
Description
A. D. Johnstone et al, Peace, A Plasma Electron and Current Experiment
Space Sci. Rev., 79,  pp 351 - 398, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
PP & SP data is generated at MSSL, then provided to UK-CDHF
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
This is PEACE PP/SP data version 3.1, produced at MSSL
Based on onboard moments but using corrected geometric factors which account for
uplinked changes of the values used in onboard calibration as well as estimated
changes due to variable MCP gain performance
Onboard moments are calculated for up to three energy ranges. Photoelectron
contamination may affect 0, 1 or 2 of these ranges
EFW PP probe-spacecraft potential was used to select the energy ranges to be
excluded to remove misleading photoelectron contributions. Note that the density
may be underestimated if there are both plasma electrons and photoelectrons in
the lowest energy range
When 88h58 is used for the HEEA sensor, sometimes the entire plasma electron
population and photoelectrons are in just the lowest of the 3 energy ranges.
This data has been deleted in this release of the PEACE PPs
Data is deleted if the spacecraft electric potential is too large for the simple
correction procedure to work or there is no EFW PP data available
Measured electron energies have not been corrected for their acceleration by the
spacecraft electric potential
Onboard moments use onboard energy tables, efficiencies and response surfaces.
Any errors in these parameters cannot be corrected in ground data processing
Before 2001-09-11 the onboard energy efficiencies were not accurate, which
caused the density in the solar wind to be overestimated. This data has been
removed in this release of the PEACE PPs
The calculation of T_par, T_perp and Q_par used PP FGM data
The data is for context and information only. It is not suitable for detailed
analysis, but may be used for event selection
The next iteration of PP/SP moments will be of a higher quality
Please see links under
http://www.mssl.ucl.ac.uk/www_plasma/missions/cluster/clusterII.html for more
information
Please contact the PEACE PI to request science quality data
Automatically validated by UKCDC
Product delivered pre-validated by the PI institute
 
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C2_PP_RAP (spase://ESA/NumericalData/Cluster-Salsa/RAPID/PrimeParameter/PT4S)
Description
B. Wilken et al, RAPID, The Imaging Energetic Particle Spectrometer on Cluster
Space Sci. Rev., 79,  pp 399 - 473, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data processed on 2024-11-14T07:34:19Z
Caveats file: RAP_CAV_C2_V245.DAT; Release Sep 16, 2024
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
2024-02-01T03:57:00.000Z/9999-12-31T23:59:59.000Z: RAPID permanently turned off
as of Feb 1, 2024
Corrected time stamps for ions and electrons.
Energy threshold shifts have been applied.
 
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C2_PP_STA (spase://ESA/NumericalData/Cluster-Salsa/STAFF/PrimeParameter/PT4S)
Description
N. Cornilleau et al,
The Cluster Spatio-Temporal Analysis of Field Fluctuations (Staff) Experiment
Space Sci. Rev., 79,  pp 107 - 136, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
PI Software Version 4.2, 25 September 2006
 
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C2_PP_WHI (spase://ESA/NumericalData/Cluster-Salsa/WHISPER/PrimeParameter/PT4S)
Description
P. M. E. Decreau et al, WHISPER, A Resonance Sounder and Wave Analyser:
Performances and Perspectives for the Cluster Mission
Space Sci. Rev., 79,  pp 157 - 193, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Two types of parameters are provided by WHISPER:
1) Density values (and quality): N_e_res and N_e_res_q, are related to sounding
operations.
The N_e_res value is calculated from an algorithm for resonance recognition,
which cannot take account of all level of information available to the
experimenter. The reliability of N_e_res parameters derived at the CSDS level
is thus limited in an unknown manner.
The N_e_res_q parameter (one value for each N_e_res data point) provides a crude
idea of the probability that the N_e_res value is actually correct. A value of
0 means that the value is probably wrong, a value above 80 that it is probably
correct. Anything in between reflects a crude evaluation of the chances. Refer
to PI for details.
2) Wave power values: E_pow_f4, E_pow_f5, E_pow_f6, E_pow_su and E_var_ts, are
related to recording of natural wave emissions.
Those parameters, not affected by variations in instrument's transfer functions,
are globally OK.
However, two factors can affect the precision of the measurements:
a) the occasional presence of spurious emissions created by operations of the
EDI instrument increases the wave power values measured on SC1, SC2 and SC3,
from an unknown amount,
b) the limited dynamical range of the instrument leads to an underestimation of
the E_pow parameters values when the voltage difference measured by the double
sphere antenna signal in the 2 - 80 kHz band is higher than 150 mVp or 600 mVp
(depending of the gain chosen). As a consequence, high values have to be taken
with special caution.
 
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C2_UP_FGM (spase://ESA/NumericalData/Cluster-Salsa/FGM/UnvalidatedParameter/PT4S)
Description
A. Balogh et al, The Cluster Magnetic Field Investigation
Space Sci. Rev., 79,  pp 65 - 92, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C2_UP_FGM_20240908 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
For the extended mission (starting 1/1/2006) CSDS FGM products
are not validated prior to release to the science community.
Spikes and other artefacts that were previously removed during
validation of the FGM PP/SP data may occur in these files.
 
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C2_WAVEFORM_WBD doi:10.48322/8hs9-sg97
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bands in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'cluster_wbd_calibration.pdf'. Because the calibration was applied in the time
domain using a simple equation the raw counts actually measured by the WBD
instrument can be obtained by using these equations and solving for 'Raw
Counts', keeping in mind that this number is an Integer ranging from 0 to 255. 
Since DC offset is a real number, the resultant when solving for raw counts will
need to be converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, the
following steps need to be carried out:  1) If Electric Field, first divide
calibrated data by 1000 to get V m^-1; 2) Apply window of preference, if any
(such as Hanning, etc.); 3) Divide data values by sqrt(2) to get back to the rms
domain; 4) perform FFT (see Bandwidth variable notes for non-continuous modes);
5) divide by the noise bandwidth, which is equal to the sampling frequency
divided by the FFT size (see table below for appropriate sampling frequency); 6)
multiply by the appropriate constant for the window used, if any.
...
Bandwidth   Sample Rate
---------   ------------
9.5 kHz      27.443 kHz 
19 kHz       54.886 kHz 
77 kHz      219.544 kHz 
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Mar 2008.Revised Dec 2008, Jan 2010
 
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C2_WAVEFORM_WBD_BM2 (spase://NASA/NumericalData/Cluster-Salsa/WBD/BM2/PT0.0000046S)
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bandwidths in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'CAA_EST_CR_WBD_v20.pdf'. Because the calibration was applied in the time domain
using a simple equation the raw counts actually measured by the WBD instrument
can be obtained by using these equations and solving for 'Raw Counts', keeping
in mind that this number is an Integer ranging from 0 to 255.  Since DC offset
is a real number, the resultant when solving for raw counts will need to be
converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, see
'CAA_EST_CR_WBD_v20.pdf'. The steps for converting are briefly outlined below:
1) If Electric Field, first divide calibrated data by 1000 to get V m^-1; 2)
Apply window of preference, if any (such as Hanning, etc.); 3) Divide data
values by sqrt(2) to get back to the rms domain; 4) perform FFT (see Bandwidth
VAR_NOTES for non-continuous modes); 5) divide by the noise bandwidth, which is
equal to the sampling frequency divided by the FFT size (see table in VAR_NOTES
of the 'BM_Mode' variable for the appropriate sampling frequency); 6) multiply
by the appropriate constant for the window used, if any;7) if Translation is not
equal to 0, add the appropriate translation frequency to each frequency
component (see Translation CATDESC for the exact values).
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Nov 2014.
 
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C3_CP_CIS-CODIF_H1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HE1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_H1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_H1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_HE1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_O1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_HS_O1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_O1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_PAD_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_PAD_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-CODIF_PAD_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-CODIF_CAVEATS
 
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C3_CP_CIS-HIA_HS_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_MAG_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_MAG_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_MAG_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_SW_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_SW_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_HS_SW_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_LS_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_LS_SW_IONS_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_LS_SW_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_LS_SW_IONS_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_CIS-HIA_PAD_HS_MAG_IONS_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C3_CQ_CIS-HIA_CAVEATS
 
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C3_CP_EDI_AEDC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/16 s for normal and 1/128 s for burst mode 
The AEC (*.edi_ae_cor) files were used to correct for angular (theta-phi)
dependence of the efficieny
The correction is applied to the original CDF files delivered by the EDI team
 
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C3_CP_EDI_MP
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Non-regularly spaced time-series! It contains quarter-spin, half-spin
and spin resolution data with all qualities: GOOD/CAUTION/BAD. 
The values 2/1/0 for GOOD/CAUTION/BAD are  written to Status[0].
Data from spin, half spin and quarter spin IFF files are merged by an algorithm
that can be
thought of as a 'use more if not lower quality' algorithm.
The analysis is performed on each spin's worth of data starting
with spin resolution. If there is more data of half spin 
resolution with equal or better quality, it replaces the spin
resolution data. Likewise, if there is more data of quarter 
spin resolution with equal or better quality, it replaces the
half spin resolution data.
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
DATASET VERSION HISTORY
VERSION 01: The first version of this dataset was converted by the CAA
from source CDF files provided by the EDI team. This conversion involved
insertion of a half interval parameter that was not included in the source
files and correction of missing or bad metadata. The half interval
determination was based on comparison with the spin time-tags provided
in the EDI CSDS Prime Parameter data file. In some cases a consistent
determination could not be found with the PP data and the half-interval
was set to the minimum, quarter spin, 1 second, value.
CDF to CEF Conversion was done using revision 1.1 (2006/11/06) of
edi_mp_convert.pro
Metadata correction was done using revision 1.1 (2006/11/06) of edi_fix_fatal.sh
FILE VERSION HISTORY
For this initial conversion the CAA CEF files have retained the same file
version number as the source CDF files. In most cases file versions are
V13 or V14.
VERSION 02: Minor changes
 
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C3_CP_EDI_QZC
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Mixed time resolution: 1/8 s for normal and 1/64 s for burst mode 
MIN_TIME_RESOLUTION is set to fill_value
MAX_TIME_RESOLUTION is given for BM
Not regularly spaced timeline 
The background electron counts at fixed energy and pitch angle may be
contaminated with beam electrons 
Status parameter has two bits for electron energy and acquisition time for the
electron counts
bit0=0: acquisition time=1/512 s; bit0=1: acq_time=1/1024 s 
bit1 is the energy flag=0/1 for 1/0.5 keV electron energy
 
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C3_CP_EDI_SPIN
Description
Electron Drift Instrument
Electric field measured by the drift velocity 
of monoenergetic artificial electron beams 
injected perpendicularly to the ambient magnetic field
Modification History
Spin resolution data with GOOD/CAUTION qualities.
The values 2/1 for GOOD/CAUTION are in Status[0].
The electric field and drift velocity measurements are given
in the inertial frame (a correction has been applied for the
spacecraft velocity).
 
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C3_CP_EFW_L3_E3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C3_CP_FGM_5VPS
 - CL_SP_AUX
 - C3_CP_AUX_POSGSE_1M
 
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C3_CP_EFW_L3_P
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
Level 3 quantity P is the negative of the spacecraft potential,
calculated by averaging the Level 2 quantity P over 4 seconds.
For more information on data quality and how the CAA data are processed,
please consult the EFW CAA Users Guide and the EFW CAA Interface Control
Document (ICD).
Detailed quality information is provided as a 16 bit set of flags
in the parameter P_bitmask__C3_CP_EFW_L3_P. The meaning of
the bits is as follows (LSB numbering starting at 0):
Bit  0: Reset.
Bit  1: Bad bias.
Bit  2: Probe latchup.
Bit  3: Low density saturation (-68V).
Bits 4-12: N/A
Bit 13: Whisper operating.
Bit 14: Saturation due to high bias current.
Bit 15: N/A
 
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C3_CP_EFW_L3_V3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C3_CP_FGM_5VPS
 - CL_SP_AUX
 - C3_CP_AUX_POSGSE_1M
 
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C3_CP_FGM_5VPS
Description
Each Cluster spacecraft carries an identical FGM instrument
(Fluxgate Magnetometer) to measure the DC magnetic field
vector. Each instrument, in turn, consists of two triaxial
fluxgate magnetometers and an onboard data processing unit.
The instrument samples the magnetic field at a cadence of 22 Hz
(67 Hz in Burst mode). In order to minimise the magnetic 
background of the spacecraft, one of the magnetometer sensors
 (the outboard, or OB sensor) is located at the end of one
 of the two 5 m radial booms of the spacecraft, the other 
(the inboard, or IB sensor) at 1.5 m inboard from the end 
of the boom. Since the start of the scientific operations 
on February 1, 2001, only the outboard sensor on each 
satellite has been used.
Modification History
*C3_CQ_FGM_CAVF
 
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C3_CP_FGM_SPIN (spase://ESA/NumericalData/Cluster-Samba/FGM/SpinResolution/PT4S)
Description
No TEXT global attribute value.
 
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C3_CP_RAP_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_ESPCT6
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_HSPCT
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_I3DM_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_I3DM_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_I3DM_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_ISPCT_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_ISPCT_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_PAD_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_PAD_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_PAD_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_PAD_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_RAP_PAD_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C3_CQ_RAP_CAVEATS
*C3_CP_RAP_DSETTINGS
 
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C3_CP_STA_CWF_GSE
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C3_CQ_STA_CALIB_YTR_CAVEATS
*C3_CQ_STA_NOTSRP_MTR_CAVEATS
DATASET VERSION HISTORY
Version 01: First version of dataset.
Version 02: Few corrected re-deliveries.
Version 03: Removal of on-board calibration records is now based on
the calibration bit (instead of the step-in-cal character).
 
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C3_CP_STA_PPP
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C3_CQ_STA_SA_UNDEF_MFA_TR_CAVEATS
*C3_CQ_STA_NOTSRP_MTR_CAVEATS
*C3_CQ_STA_CALIB_YTR_CAVEATS
DATASET VERSION HISTORY:
Version 09 : Reprocessed due to FGM and/or SPD-AUX files re-deliveries.
Version 08 : FGM induced gaps revised and completed.
Version 07 : New calibration tables plus addition of the half-interval 
duration and status. Removal of onboard calibration data.
Now with FGM induced gaps. FGM file used described in the FILE_CAVEATS 
metadata section. 
Warning to the users of versions lower than 07:
Delta_plus of Time__C3_CP_STA_PPP variables was set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate).
Note that the data themselves are correct.
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Version 05: used the new calibration tables (feb 2013).
Version 03: AUX files in CDF format used are 26 hours.
Same data than version02 but less missing values.
Version 02: Data format corrected.
Version 01: Obsolete. Should not be used !
 
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C3_CP_STA_PSD
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C3_CQ_STA_SA_PSD_NEG_CAVEATS
*C3_CQ_STA_NOTSRP_MTR_CAVEATS
*C3_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C3_CP_STA_PSD variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the usual minimum time resolution (1s)
which is correct in most of the time (Normal Bit Rate).
The  time resolution is better in High Bit Rate.
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
The PSD negative values in the version 03 have been replaced 
by the fillvalue (-1.00E+31).
Version 03:
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Phase rotation corrected + exhaustive data. Older versions 
are obsolete and should not be used ! The negative values must not be
taken into account by the users.
Version 02 : Obsolete. This version may be used if Version 03 is not 
available, as long as only total B and total E power are used !
Version 01 : Obsolete. Should not be used !
 
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C3_CP_STA_SM
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C3_CQ_STA_NOTSRP_MTR_CAVEATS
*C3_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C3_CP_STA_SM variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate)
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
Units and Si Conversion of the variables BB and BE have been corrected.
Version 03 : Phase rotation corrected + exhaustive data. 
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Older versions are obsolete and should not be used ! 
Version 02 : Obsolete. Should not be used !
Version 01 : Obsolete. Should not be used !
 
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C3_CP_WHI_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C3_CP_WHI_ELECTRON_DENSITY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update, QUALITY changed to CONTRAST, addition of a
new QUALITY variable
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C3_CP_WHI_NATURAL
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C3_CP_WHI_PASSIVE_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C3_CP_WHI_WAVE_FORM_ENERGY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C3_JP_PMP (spase://ESA/NumericalData/Cluster-Samba/Ephemeris/JP/PredictedMagneticPosition/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation used to calculate magnetic field and L value 
 in PMP files produced after 23 Feb 2020.
Caveats
JSOC predicted magnetic positions.
 
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C3_JP_PSE (spase://ESA/NumericalData/Cluster-Samba/Ephemeris/JP/PredictedScientificEvent/PT0.016S)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
AP _ Apogee
CY 1 Start of visibility window at Canberra (5 deg elevation)
CY 2 Start of visibility window at Canberra (5 deg elevation)
CY 3 Start of visibility window at Canberra (5 deg elevation)
CZ 1 End of visibility window at Canberra (5 deg elevation)
CZ 2 End of visibility window at Canberra (5 deg elevation)
CZ 3 End of visibility window at Canberra (5 deg elevation)
CZ 4 End of visibility window at Canberra (5 deg elevation)
DY 1 Start of visibility window at Vilspa (5 deg elevation)
DY 2 Start of visibility window at Vilspa (5 deg elevation)
DY 3 Start of visibility window at Vilspa (5 deg elevation)
DZ 1 End of visibility window at Vilspa (5 deg elevation)
DZ 2 End of visibility window at Vilspa (5 deg elevation)
DZ 3 End of visibility window at Vilspa (5 deg elevation)
GY 1 Start of visibility window at Goldstone (5 deg elevation)
GY 2 Start of visibility window at Goldstone (5 deg elevation)
GY 3 Start of visibility window at Goldstone (5 deg elevation)
GY 4 Start of visibility window at Goldstone (5 deg elevation)
GZ 1 End of visibility window at Goldstone (5 deg elevation)
GZ 2 End of visibility window at Goldstone (5 deg elevation)
GZ 3 End of visibility window at Goldstone (5 deg elevation)
JY 1 Start of visibility window at Maspalomas (5 deg elevation)
JY 2 Start of visibility window at Maspalomas (5 deg elevation)
JY 3 Start of visibility window at Maspalomas (5 deg elevation)
JY 4 Start of visibility window at Maspalomas (5 deg elevation)
JZ 1 End of visibility window at Maspalomas (5 deg elevation)
JZ 2 End of visibility window at Maspalomas (5 deg elevation)
JZ 3 End of visibility window at Maspalomas (5 deg elevation)
KA 1 Start of visibility window at Kourou (5 deg elevation)
KA 2 Start of visibility window at Kourou (5 deg elevation)
KA 3 Start of visibility window at Kourou (5 deg elevation)
KA 4 Start of visibility window at Kourou (5 deg elevation)
KL 1 End of visibility window at Kourou (5 deg elevation)
KL 2 End of visibility window at Kourou (5 deg elevation)
KL 3 End of visibility window at Kourou (5 deg elevation)
KL 4 End of visibility window at Kourou (5 deg elevation)
MY 1 Start of visibility window at Madrid (5 deg elevation)
MY 2 Start of visibility window at Madrid (5 deg elevation)
MY 3 Start of visibility window at Madrid (5 deg elevation)
MY 4 Start of visibility window at Madrid (5 deg elevation)
MZ 1 End of visibility window at Madrid (5 deg elevation)
MZ 2 End of visibility window at Madrid (5 deg elevation)
MZ 3 End of visibility window at Madrid (5 deg elevation)
NS S Southbound neutral sheet
NT I Enter north tail lobe from inner magnetosphere
PA 1 Start of visibility window at Perth (5 deg elevation)
PA 2 Start of visibility window at Perth (5 deg elevation)
PA 3 Start of visibility window at Perth (5 deg elevation)
PE _ Perigee
PL 1 End of visibility window at Perth (5 deg elevation)
PL 2 End of visibility window at Perth (5 deg elevation)
PL 3 End of visibility window at Perth (5 deg elevation)
PL 4 End of visibility window at Perth (5 deg elevation)
QL I Inbound critical L value for auroral zone
QL O Outbound critical L value for auroral zone
RA 1 Start of visibility window at Redu (5 deg elevation)
RA 2 Start of visibility window at Redu (5 deg elevation)
RA 3 Start of visibility window at Redu (5 deg elevation)
RA 4 Start of visibility window at Redu (5 deg elevation)
RL 1 End of visibility window at Redu (5 deg elevation)
RL 2 End of visibility window at Redu (5 deg elevation)
RL 3 End of visibility window at Redu (5 deg elevation)
ST O Leave south tail lobe for inner magnetosphere
TL I Inbound radiation belt entry for WEC
TL O Outbound radiation belt exit for WEC
VL I Inbound critical L value for EDI
VL O Outbound critical L value for EDI
WL I Inbound critical L value for ASPOC
WL O Outbound critical L value for ASPOC
XL I Inbound critical L value for PEACE
XL O Outbound critical L value for PEACE
YL I Inbound critical L value for RAPID
YL O Outbound critical L value for RAPID
ZL I Inbound critical L value for CIS
ZL O Outbound critical L value for CIS
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate GSM latitude and MLT 
 in PSE files produced after 23 Feb 2020.
PSE files updated to support orbits >999 and six decimal figures 
 on orbit phase from 25 March 2006.
Caveats
JSOC predicted scientific events.
 
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C3_PP_ASP (spase://ESA/NumericalData/Cluster-Samba/ASPOC/PrimeParameter/PT4S)
Description
K. Torkar et al, Active spacecraft potential control for Cluster -
implementation and first results
Ann. Geophys., 19,  pp 1289 - 1302, 2001)
Modification History
none
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
One raw data format (5.1.5 secs) of bad data may occur
when the instrument is powered on.
 
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C3_PP_CIS (spase://ESA/NumericalData/Cluster-Samba/CIS/PrimeParameter/PT4S)
Description
H. Reme et al, First multispacecraft ion measurements in and near 
the Earth's magnetosphere with the identical 
Cluster Ion Spectrometry (CIS) experiment
Annales Geophysicae, 19, pp 1303 - 1354, 2001
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C3_PP_CIS_20211231 pre-validated by CIS team and supplied to UKCDC for inges
The user of the CIS data needs to be cautious.
Please refer to the CIS Home Page:
http://cluster.irap.omp.eu/index.php?page=caveats ,
link [Caveats for specific data intervals], for caveats concerning these data.
 
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C3_PP_EDI doi:10.48322/pn1d-v155
Description
G. Paschmann et al, The Electron Drift Instrument for Cluster
Space Sci. Rev., 79,  pp 233 - 269, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
1) EDI's automated analysis algorithm has a known susceptibility to
producing occasional incorrect values of the drift velocities (and electric
fields). The code attempts to prevent these bad values to be output
to the cdf file. No further removal is done in the validation process.
2) When drift velocities become sufficiently large, there can be a
180-degree ambiguity in drift direction that is usually flagged in bit 7
(counting from 0) of Status Byte 3.
3) There are two methods to analyze a spin's worth of EDI data. If bits 5 &
6 in Status Byte 3 are NOT set, the employed method was triangulation. If
either bit 5 or 6 are set, then the results are from time-of-flight
analysis.
4) The reported drift velocities and electric field refer to inertial
coordinates, i.e., have been corrected for spacecraft velocity. However, the
magnitude errors (in %) and the angle errors (in degrees), reported in
Status Bytes 5 & 6, respectively, refer to the spacecraft frame and have NOT
yet been converted to inertial coordinates.
5) The reduced chi-square reported as a data word is a measure of the
goodness-of-fit of the triangulation analysis.
 
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C3_PP_EFW (spase://ESA/NumericalData/Cluster-Samba/EFW/PrimeParameter/PT4S)
Description
G. Gustafsson et al, The Electric Field and Wave Experiment for Cluster
Space Sci. Rev., 79,  pp 137 - 156, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data calibration may be unreliable at this early stage of the mission
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** CSDS data are not for publication ***
Be aware that data may be reprocessed as necessary to improve quality
For questions on data validity please contact sdc-adm@plasma.kth.se
Fill value inserted for E_dusk__C3_PP_EFW: No reason given
for time range 2024-09-01T00:00:00Z to 2024-10-01T00:00:00Z
Fill value inserted for E_pow_f1__C3_PP_EFW: No reason given
for time range 2024-09-01T00:00:00Z to 2024-10-01T00:00:00Z
Fill value inserted for E_sigma__C3_PP_EFW: No reason given
for time range 2024-09-01T00:00:00Z to 2024-10-01T00:00:00Z
Fill value inserted for U_probe_sc__C3_PP_EFW: No reason given
for time range 2024-09-01T00:00:00Z to 2024-10-01T00:00:00Z
 
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C3_PP_PEA (spase://ESA/NumericalData/Cluster-Samba/PEACE/PrimeParameter/PT4S)
Description
A. D. Johnstone et al, Peace, A Plasma Electron and Current Experiment
Space Sci. Rev., 79,  pp 351 - 398, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
PP & SP data is generated at MSSL, then provided to UK-CDHF
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
This is PEACE PP/SP data version 3.1, produced at MSSL
Based on onboard moments but using corrected geometric factors which account for
uplinked changes of the values used in onboard calibration as well as estimated
changes due to variable MCP gain performance
Onboard moments are calculated for up to three energy ranges. Photoelectron
contamination may affect 0, 1 or 2 of these ranges
EFW PP probe-spacecraft potential was used to select the energy ranges to be
excluded to remove misleading photoelectron contributions. Note that the density
may be underestimated if there are both plasma electrons and photoelectrons in
the lowest energy range
When 88h58 is used for the HEEA sensor, sometimes the entire plasma electron
population and photoelectrons are in just the lowest of the 3 energy ranges.
This data has been deleted in this release of the PEACE PPs
Data is deleted if the spacecraft electric potential is too large for the simple
correction procedure to work or there is no EFW PP data available
Measured electron energies have not been corrected for their acceleration by the
spacecraft electric potential
Onboard moments use onboard energy tables, efficiencies and response surfaces.
Any errors in these parameters cannot be corrected in ground data processing
Before 2001-09-11 the onboard energy efficiencies were not accurate, which
caused the density in the solar wind to be overestimated. This data has been
removed in this release of the PEACE PPs
The calculation of T_par, T_perp and Q_par used PP FGM data
The data is for context and information only. It is not suitable for detailed
analysis, but may be used for event selection
The next iteration of PP/SP moments will be of a higher quality
Please see links under
http://www.mssl.ucl.ac.uk/www_plasma/missions/cluster/clusterII.html for more
information
Please contact the PEACE PI to request science quality data
Automatically validated by UKCDC
Product delivered pre-validated by the PI institute
 
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C3_PP_RAP (spase://ESA/NumericalData/Cluster-Samba/RAPID/PrimeParameter/PT4S)
Description
B. Wilken et al, RAPID, The Imaging Energetic Particle Spectrometer on Cluster
Space Sci. Rev., 79,  pp 399 - 473, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data processed on 2024-11-14T07:34:19Z
Caveats file: RAP_CAV_C3_V245.DAT; Release Sep 16, 2024
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Corrected time stamps for ions and electrons.
Energy threshold shifts have been applied.
Solar noise removed from electrons.
Changed EDB format, on-board anisotropies not possible in NM
 
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C3_PP_STA (spase://ESA/NumericalData/Cluster-Samba/STAFF/PrimeParameter/PT4S)
Description
N. Cornilleau et al,
The Cluster Spatio-Temporal Analysis of Field Fluctuations (Staff) Experiment
Space Sci. Rev., 79,  pp 107 - 136, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
PI Software Version 4.2, 25 September 2006
 
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C3_PP_WHI (spase://ESA/NumericalData/Cluster-Samba/WHISPER/PrimeParameter/PT4S)
Description
P. M. E. Decreau et al, WHISPER, A Resonance Sounder and Wave Analyser:
Performances and Perspectives for the Cluster Mission
Space Sci. Rev., 79,  pp 157 - 193, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Two types of parameters are provided by WHISPER:
1) Density values (and quality): N_e_res and N_e_res_q, are related to sounding
operations.
The N_e_res value is calculated from an algorithm for resonance recognition,
which cannot take account of all level of information available to the
experimenter. The reliability of N_e_res parameters derived at the CSDS level
is thus limited in an unknown manner.
The N_e_res_q parameter (one value for each N_e_res data point) provides a crude
idea of the probability that the N_e_res value is actually correct. A value of
0 means that the value is probably wrong, a value above 80 that it is probably
correct. Anything in between reflects a crude evaluation of the chances. Refer
to PI for details.
2) Wave power values: E_pow_f4, E_pow_f5, E_pow_f6, E_pow_su and E_var_ts, are
related to recording of natural wave emissions.
Those parameters, not affected by variations in instrument's transfer functions,
are globally OK.
However, two factors can affect the precision of the measurements:
a) the occasional presence of spurious emissions created by operations of the
EDI instrument increases the wave power values measured on SC1, SC2 and SC3,
from an unknown amount,
b) the limited dynamical range of the instrument leads to an underestimation of
the E_pow parameters values when the voltage difference measured by the double
sphere antenna signal in the 2 - 80 kHz band is higher than 150 mVp or 600 mVp
(depending of the gain chosen). As a consequence, high values have to be taken
with special caution.
 
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C3_UP_FGM (spase://ESA/NumericalData/Cluster-Samba/FGM/UnvalidatedParameter/PT4S)
Description
A. Balogh et al, The Cluster Magnetic Field Investigation
Space Sci. Rev., 79,  pp 65 - 92, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C3_UP_FGM_20240930 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
For the extended mission (starting 1/1/2006) CSDS FGM products
are not validated prior to release to the science community.
Spikes and other artefacts that were previously removed during
validation of the FGM PP/SP data may occur in these files.
 
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C3_WAVEFORM_WBD doi:10.48322/y123-4274
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bands in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'cluster_wbd_calibration.pdf'. Because the calibration was applied in the time
domain using a simple equation the raw counts actually measured by the WBD
instrument can be obtained by using these equations and solving for 'Raw
Counts', keeping in mind that this number is an Integer ranging from 0 to 255. 
Since DC offset is a real number, the resultant when solving for raw counts will
need to be converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, the
following steps need to be carried out:  1) If Electric Field, first divide
calibrated data values by 1000 to get V/m; 2) Apply window of preference, if any
(such as Hanning, etc.); 3) Divide data values by sqrt(2) to get back to the rms
domain; 4) perform FFT (see Bandwidth variable notes for non-continuous modes);
5) divide by the noise bandwidth, which is equal to the sampling frequency
divided by the FFT size (see table below for appropriate sampling frequency); 6)
multiply by the appropriate constant for the window used, if any.
...
Bandwidth   Sample Rate
---------   ------------
9.5 kHz      27.443 kHz 
19 kHz       54.886 kHz 
77 kHz      219.544 kHz 
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Mar 2008.Revised Dec 2008, Jan 2010
 
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C3_WAVEFORM_WBD_BM2 (spase://NASA/NumericalData/Cluster-Samba/WBD/BM2/PT0.0000046S)
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bandwidths in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'CAA_EST_CR_WBD_v20.pdf'. Because the calibration was applied in the time domain
using a simple equation the raw counts actually measured by the WBD instrument
can be obtained by using these equations and solving for 'Raw Counts', keeping
in mind that this number is an Integer ranging from 0 to 255.  Since DC offset
is a real number, the resultant when solving for raw counts will need to be
converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, see
'CAA_EST_CR_WBD_v20.pdf'. The steps for converting are briefly outlined below:
1) If Electric Field, first divide calibrated data by 1000 to get V m^-1; 2)
Apply window of preference, if any (such as Hanning, etc.); 3) Divide data
values by sqrt(2) to get back to the rms domain; 4) perform FFT (see Bandwidth
VAR_NOTES for non-continuous modes); 5) divide by the noise bandwidth, which is
equal to the sampling frequency divided by the FFT size (see table in VAR_NOTES
of the 'BM_Mode' variable for the appropriate sampling frequency); 6) multiply
by the appropriate constant for the window used, if any;7) if Translation is not
equal to 0, add the appropriate translation frequency to each frequency
component (see Translation CATDESC for the exact values).
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Nov 2014.
 
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C4_CP_CIS-CODIF_H1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HE1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HE1_DENSITY_CORRECTED
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
 
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C4_CP_CIS-CODIF_HS_H1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_H1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_HE1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_O1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_HS_O1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_H1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_H1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_HE1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_O1_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_LS_O1_PSD
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_O1_1D_PEF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_HS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_HS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_HS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_LS_H1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_LS_HE1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_CIS-CODIF_PAD_LS_O1_PF
Description
Cluster Ion Spectrometry.
The CIS (Cluster Ion Spectrometry) experiment is a comprehensive
ionic plasma spectrometry package onboard the Cluster spacecraft,
capable of obtaining full three-dimentional ion distributions
(about 0 to 40 keV/e) with a time resolution of one spacecraft spin (4 sec)
and with mass-per-charge composition determination.
The CIS package consists of two different instruments,
a time-of-flight ion Composition and Distribution Function analyser (CODIF, or
CIS-1)
and a Hot Ion Analyser (HIA, or CIS-2).
Modification History
*C4_CQ_CIS-CODIF_CAVEATS
 
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C4_CP_EFW_L3_E3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C4_CP_FGM_5VPS
 - CL_SP_AUX
 - C4_CP_AUX_POSGSE_1M
 
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C4_CP_EFW_L3_P
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
Level 3 quantity P is the negative of the spacecraft potential,
calculated by averaging the Level 2 quantity P over 4 seconds.
For more information on data quality and how the CAA data are processed,
please consult the EFW CAA Users Guide and the EFW CAA Interface Control
Document (ICD).
Detailed quality information is provided as a 16 bit set of flags
in the parameter P_bitmask__C4_CP_EFW_L3_P. The meaning of
the bits is as follows (LSB numbering starting at 0):
Bit  0: Reset.
Bit  1: Bad bias.
Bit  2: Probe latchup.
Bit  3: Low density saturation (-68V).
Bits 4-12: N/A
Bit 13: Whisper operating.
Bit 14: Saturation due to high bias current.
Bit 15: N/A
 
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C4_CP_EFW_L3_V3D_INERT
Description
The EFW (Electric Field and Wave) instrument consists of four spherical
probes deployed orthogonally on 44-meter-long wire booms in the spin
plane of the spacecraft. The potential differences between opposing
probes, separated by 88 m tip-to-tip, are measured to provide electric
field measurements in two directions, thus providing the full electric
field vector in the spin plane of the spacecraft. Additionally, the
potential differences between each of the probes and the spacecraft are
measured, providing an estimate of the spacecraft potential relative
to the plasma, which can be used as a proxy for the ambient electron
density. The output analogue signals from the preamplifiers connected
to the spherical probes are also provided to the wave instruments
(STAFF, WHISPER and WBD) for analysis of high frequency wave phenomena.
Modification History
This dataset has been calculated using the following products:
 - C4_CP_FGM_5VPS
 - CL_SP_AUX
 - C4_CP_AUX_POSGSE_1M
 
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C4_CP_FGM_5VPS
Description
Each Cluster spacecraft carries an identical FGM instrument
(Fluxgate Magnetometer) to measure the DC magnetic field
vector. Each instrument, in turn, consists of two triaxial
fluxgate magnetometers and an onboard data processing unit.
The instrument samples the magnetic field at a cadence of 22 Hz
(67 Hz in Burst mode). In order to minimise the magnetic 
background of the spacecraft, one of the magnetometer sensors
 (the outboard, or OB sensor) is located at the end of one
 of the two 5 m radial booms of the spacecraft, the other 
(the inboard, or IB sensor) at 1.5 m inboard from the end 
of the boom. Since the start of the scientific operations 
on February 1, 2001, only the outboard sensor on each 
satellite has been used.
Modification History
*C4_CQ_FGM_CAVF
 
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C4_CP_FGM_SPIN (spase://ESA/NumericalData/Cluster-Tango/FGM/SpinResolution/PT4S)
Description
No TEXT global attribute value.
 
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C4_CP_RAP_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_ESPCT6
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_HSPCT
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_I3DM_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_I3DM_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_I3DM_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_ISPCT_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_ISPCT_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_PAD_CNO
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_PAD_E3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_PAD_H
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_PAD_HE
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_RAP_PAD_L3DD
Description
Research with Adaptive Particle Imaging Detectors (RAPID)
The RAPID spectrometer for the Cluster mission is an
advanced particle detector for the analysis of suprathermal
plasma distributions in the energy range from 39-400 keV
for electrons, 28-1500 keV (4000 keV) for hydrogen,
and 10 keV/nuc - 1500 keV (4000 keV) for heavier ions.
Modification History
*C4_CQ_RAP_CAVEATS
*C4_CP_RAP_DSETTINGS
 
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C4_CP_STA_CWF_GSE
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C4_CQ_STA_CALIB_YTR_CAVEATS
*C4_CQ_STA_NOTSRP_MTR_CAVEATS
DATASET VERSION HISTORY
Version 01: First version of dataset.
Version 02: Few corrected re-deliveries.
Version 03: Removal of on-board calibration records is now based on
the calibration bit (instead of the step-in-cal character).
 
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C4_CP_STA_PPP
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C4_CQ_STA_SA_UNDEF_MFA_TR_CAVEATS
*C4_CQ_STA_NOTSRP_MTR_CAVEATS
*C4_CQ_STA_CALIB_YTR_CAVEATS
DATASET VERSION HISTORY:
Version 09 : Reprocessed due to FGM and/or SPD-AUX files re-deliveries.
Version 08 : FGM induced gaps revised and completed.
Version 07 : New calibration tables plus addition of the half-interval 
duration and status. Removal of onboard calibration data.
Now with FGM induced gaps. FGM file used described in the FILE_CAVEATS 
metadata section. 
Warning to the users of versions lower than 07:
Delta_plus of Time__C4_CP_STA_PPP variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate).
Note that the data themselves are correct.
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Version 05: used the new calibration tables (feb 2013).
Version 03: AUX files in CDF format used are 26 hours.
Same data than version02 but less missing values.
Version 02: Data format corrected.
Version 01: Obsolete. Should not be used !
 
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C4_CP_STA_PSD
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C4_CQ_STA_SA_PSD_NEG_CAVEATS
*C4_CQ_STA_NOTSRP_MTR_CAVEATS
*C4_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C4_CP_STA_PSD variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the usual minimum time resolution (1s)
which is correct in most of the time (Normal Bit Rate).
The  time resolution is better in High Bit Rate.
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
The PSD negative values in the version 03 have been replaced 
by the fillvalue (-1.00E+31).
Version 03:
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Phase rotation corrected + exhaustive data. Older versions 
are obsolete and should not be used ! The negative values must not be
taken into account by the users.
Version 02 : Obsolete. This version may be used if Version 03 is not 
available, as long as only total B and total E power are used !
Version 01 : Obsolete. Should not be used !
 
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C4_CP_STA_SM
Description
STAFF (Spatio Temporal Analysis of Field Fluctuations) is one of the five
experiments 
of the Wave Experiment Consortium (WEC).
The STAFF experiment comprises a boom-mounted three-axis search coil
magnetometer to 
measure magnetic fluctuations in the frequency range 0.1 Hz  - 4 kHz, a 
preamplifier and an electronics box that houses the two complementary 
data-analysis packages: a digital Spectrum Analyser, and an on-board waveform 
unit (SC).
Modification History
*C4_CQ_STA_NOTSRP_MTR_CAVEATS
*C4_CQ_STA_CALIB_YTR_CAVEATS
Version 07 : New calibration tables plus addition of the interval 
duration and status. Removal of onboard calibration data.
Warning to the users of versions lower than 07:
Delta_plus of Time__C4_CP_STA_SM variables is set to a fixed value
instead of a value varying with the mode.
This chosen fixed value is the minimum time resolution (4s)
which is correct in most of the cases (Normal Bit Rate)
Note that the data themselves are correct.
Version 04 : All the headers have been updated (laboratory name 
and email). Introduction of a new header file (Dataset). 
Units and Si Conversion of the variables BB and BE have been corrected.
Version 03 : Phase rotation corrected + exhaustive data. 
The data were time tagged using TED version 2.4.3
(TED Library 4.4.3 User Patch 1), provided by the Sheffield DWP Group.
Older versions are obsolete and should not be used ! 
Version 02 : Obsolete. Should not be used !
Version 01 : Obsolete. Should not be used !
 
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C4_CP_WHI_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C4_CP_WHI_ELECTRON_DENSITY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update, QUALITY changed to CONTRAST, addition of a
new QUALITY variable
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C4_CP_WHI_NATURAL
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C4_CP_WHI_PASSIVE_ACTIVE
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: correction of the Spectral Frequencies parameter description
VERSION 03: dataset headers update
VERSION 04: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 05: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C4_CP_WHI_WAVE_FORM_ENERGY
Description
The Wave of HIgh frequency and Sounder for Probing of Electron density
by Relaxation (WHISPER) performs the measurement of the electron density
on the four satellites of the CLUSTER project. The two main purposes of
the WHISPER experiment are to record the natural waves and to make a
diagnostic of the electron density using the sounding technique.
The various working modes and the fourier transforms calculated on board
provide a good frequency resolution obtained in the bandwidth 2-83 kHz.
Onboard data compression by the Digital Wave Processing (DWP) intrument
allows a good dynamic and level resolution of the electric signal amplitude.
Modification History
DATASET VERSION HISTORY
VERSION 01: first version of dataset
VERSION 02: dataset headers update
VERSION 03: TIME_RESOLUTION, VERSION_NUMBER, DATASET_TYPE metadata update - Aug
2020
VERSION 04: CONTACT_COORDINATES and ACKNOWLEDGEMENT metadata update - Mar 2022
 
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C4_JP_PMP (spase://ESA/NumericalData/Cluster-Tango/Ephemeris/JP/PredictedMagneticPosition/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation used to calculate magnetic field and L value 
 in PMP files produced after 23 Feb 2020.
Caveats
JSOC predicted magnetic positions.
 
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C4_JP_PSE (spase://ESA/NumericalData/Cluster-Tango/Ephemeris/JP/PredictedScientificEvent/PT0.016S)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
AP _ Apogee
CY 1 Start of visibility window at Canberra (5 deg elevation)
CY 2 Start of visibility window at Canberra (5 deg elevation)
CY 3 Start of visibility window at Canberra (5 deg elevation)
CZ 1 End of visibility window at Canberra (5 deg elevation)
CZ 2 End of visibility window at Canberra (5 deg elevation)
CZ 3 End of visibility window at Canberra (5 deg elevation)
CZ 4 End of visibility window at Canberra (5 deg elevation)
DY 1 Start of visibility window at Vilspa (5 deg elevation)
DY 2 Start of visibility window at Vilspa (5 deg elevation)
DY 3 Start of visibility window at Vilspa (5 deg elevation)
DY 4 Start of visibility window at Vilspa (5 deg elevation)
DZ 1 End of visibility window at Vilspa (5 deg elevation)
DZ 2 End of visibility window at Vilspa (5 deg elevation)
DZ 3 End of visibility window at Vilspa (5 deg elevation)
GY 1 Start of visibility window at Goldstone (5 deg elevation)
GY 2 Start of visibility window at Goldstone (5 deg elevation)
GY 3 Start of visibility window at Goldstone (5 deg elevation)
GY 4 Start of visibility window at Goldstone (5 deg elevation)
GZ 1 End of visibility window at Goldstone (5 deg elevation)
GZ 2 End of visibility window at Goldstone (5 deg elevation)
GZ 3 End of visibility window at Goldstone (5 deg elevation)
JY 1 Start of visibility window at Maspalomas (5 deg elevation)
JY 2 Start of visibility window at Maspalomas (5 deg elevation)
JY 3 Start of visibility window at Maspalomas (5 deg elevation)
JY 4 Start of visibility window at Maspalomas (5 deg elevation)
JZ 1 End of visibility window at Maspalomas (5 deg elevation)
JZ 2 End of visibility window at Maspalomas (5 deg elevation)
JZ 3 End of visibility window at Maspalomas (5 deg elevation)
KA 1 Start of visibility window at Kourou (5 deg elevation)
KA 2 Start of visibility window at Kourou (5 deg elevation)
KA 3 Start of visibility window at Kourou (5 deg elevation)
KA 4 Start of visibility window at Kourou (5 deg elevation)
KL 1 End of visibility window at Kourou (5 deg elevation)
KL 2 End of visibility window at Kourou (5 deg elevation)
KL 3 End of visibility window at Kourou (5 deg elevation)
KL 4 End of visibility window at Kourou (5 deg elevation)
MY 1 Start of visibility window at Madrid (5 deg elevation)
MY 2 Start of visibility window at Madrid (5 deg elevation)
MY 3 Start of visibility window at Madrid (5 deg elevation)
MY 4 Start of visibility window at Madrid (5 deg elevation)
MZ 1 End of visibility window at Madrid (5 deg elevation)
MZ 2 End of visibility window at Madrid (5 deg elevation)
MZ 3 End of visibility window at Madrid (5 deg elevation)
NS S Southbound neutral sheet
NT I Enter north tail lobe from inner magnetosphere
PA 1 Start of visibility window at Perth (5 deg elevation)
PA 2 Start of visibility window at Perth (5 deg elevation)
PA 3 Start of visibility window at Perth (5 deg elevation)
PA 4 Start of visibility window at Perth (5 deg elevation)
PE _ Perigee
PL 1 End of visibility window at Perth (5 deg elevation)
PL 2 End of visibility window at Perth (5 deg elevation)
PL 3 End of visibility window at Perth (5 deg elevation)
PL 4 End of visibility window at Perth (5 deg elevation)
PL 5 End of visibility window at Perth (5 deg elevation)
QL I Inbound critical L value for auroral zone
QL O Outbound critical L value for auroral zone
RA 1 Start of visibility window at Redu (5 deg elevation)
RA 2 Start of visibility window at Redu (5 deg elevation)
RA 3 Start of visibility window at Redu (5 deg elevation)
RL 1 End of visibility window at Redu (5 deg elevation)
RL 2 End of visibility window at Redu (5 deg elevation)
RL 3 End of visibility window at Redu (5 deg elevation)
ST O Leave south tail lobe for inner magnetosphere
TL I Inbound radiation belt entry for WEC
TL O Outbound radiation belt exit for WEC
VL I Inbound critical L value for EDI
VL O Outbound critical L value for EDI
WL B Outbound critical L value 2 for ASPOC
WL I Inbound critical L value for ASPOC
WL O Outbound critical L value for ASPOC
XL I Inbound critical L value for PEACE
XL O Outbound critical L value for PEACE
YL I Inbound critical L value for RAPID
YL O Outbound critical L value for RAPID
ZL I Inbound critical L value for CIS
ZL O Outbound critical L value for CIS
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate GSM latitude and MLT 
 in PSE files produced after 23 Feb 2020.
PSE files updated to support orbits >999 and six decimal figures 
 on orbit phase from 25 March 2006.
Caveats
JSOC predicted scientific events.
 
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C4_PP_ASP (spase://ESA/NumericalData/Cluster-Tango/ASPOC/PrimeParameter/PT4S)
Description
K. Torkar et al, Active spacecraft potential control for Cluster -
implementation and first results
Ann. Geophys., 19,  pp 1289 - 1302, 2001)
Modification History
none
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
One raw data format (5.1.5 secs) of bad data may occur
when the instrument is powered on.
 
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C4_PP_CIS (spase://ESA/NumericalData/Cluster-Tango/CIS/PrimeParameter/PT4S)
Description
H. Reme et al, First multispacecraft ion measurements in and near 
the Earth's magnetosphere with the identical 
Cluster Ion Spectrometry (CIS) experiment
Annales Geophysicae, 19, pp 1303 - 1354, 2001
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C4_PP_CIS_20240930 pre-validated by CIS team and supplied to UKCDC for inges
The user of the CIS data needs to be cautious.
Please refer to the CIS Home Page:
http://cluster.irap.omp.eu/index.php?page=caveats ,
link [Caveats for specific data intervals], for caveats concerning these data.
 
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C4_PP_DWP (spase://ESA/NumericalData/Cluster-Tango/DWP/PrimeParameter/PT4S)
Description
L. J. C. Woolliscroft et al, The Digital Wave-Processing Experiment on Cluster
Space Sci. Rev., 79,  pp 209 - 231, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C4_PP_DWP_20220701 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
This CSDS DWP product has not been validated prior to release.
 
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C4_PP_EDI doi:10.48322/9srb-jb74
Description
G. Paschmann et al, The Electron Drift Instrument for Cluster
Space Sci. Rev., 79,  pp 233 - 269, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
C4 EDI switched off
 
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C4_PP_EFW (spase://ESA/NumericalData/Cluster-Tango/EFW/PrimeParameter/PT4S)
Description
G. Gustafsson et al, The Electric Field and Wave Experiment for Cluster
Space Sci. Rev., 79,  pp 137 - 156, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data calibration may be unreliable at this early stage of the mission
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** CSDS data are not for publication ***
Be aware that data may be reprocessed as necessary to improve quality
For questions on data validity please contact sdc-adm@plasma.kth.se
Fill value inserted for E_dusk__C4_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_pow_f1__C4_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_sigma__C4_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for U_probe_sc__C4_PP_EFW: No reason given
for time range 2024-09-30T12:05:00Z to 2024-09-30T12:08:00Z
Fill value inserted for E_dusk__C4_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for E_pow_f1__C4_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for E_sigma__C4_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
Fill value inserted for U_probe_sc__C4_PP_EFW: No reason given
for time range 2024-09-30T23:28:00Z to 2024-09-30T23:31:00Z
 
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C4_PP_PEA (spase://ESA/NumericalData/Cluster-Tango/PEACE/PrimeParameter/PT4S)
Description
A. D. Johnstone et al, Peace, A Plasma Electron and Current Experiment
Space Sci. Rev., 79,  pp 351 - 398, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
PP & SP data is generated at MSSL, then provided to UK-CDHF
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
This is PEACE PP/SP data version 3.1, produced at MSSL
Based on onboard moments but using corrected geometric factors which account for
uplinked changes of the values used in onboard calibration as well as estimated
changes due to variable MCP gain performance
Onboard moments are calculated for up to three energy ranges. Photoelectron
contamination may affect 0, 1 or 2 of these ranges
EFW PP probe-spacecraft potential was used to select the energy ranges to be
excluded to remove misleading photoelectron contributions. Note that the density
may be underestimated if there are both plasma electrons and photoelectrons in
the lowest energy range
When 88h58 is used for the HEEA sensor, sometimes the entire plasma electron
population and photoelectrons are in just the lowest of the 3 energy ranges.
This data has been deleted in this release of the PEACE PPs
Data is deleted if the spacecraft electric potential is too large for the simple
correction procedure to work or there is no EFW PP data available
Measured electron energies have not been corrected for their acceleration by the
spacecraft electric potential
Onboard moments use onboard energy tables, efficiencies and response surfaces.
Any errors in these parameters cannot be corrected in ground data processing
Before 2001-09-11 the onboard energy efficiencies were not accurate, which
caused the density in the solar wind to be overestimated. This data has been
removed in this release of the PEACE PPs
The calculation of T_par, T_perp and Q_par used PP FGM data
The data is for context and information only. It is not suitable for detailed
analysis, but may be used for event selection
The next iteration of PP/SP moments will be of a higher quality
Please see links under
http://www.mssl.ucl.ac.uk/www_plasma/missions/cluster/clusterII.html for more
information
Please contact the PEACE PI to request science quality data
Automatically validated by UKCDC
Product delivered pre-validated by the PI institute
 
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C4_PP_RAP (spase://ESA/NumericalData/Cluster-Tango/RAPID/PrimeParameter/PT4S)
Description
B. Wilken et al, RAPID, The Imaging Energetic Particle Spectrometer on Cluster
Space Sci. Rev., 79,  pp 399 - 473, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Data processed on 2024-11-14T07:34:21Z
Caveats file: RAP_CAV_C4_V245.DAT; Release Sep 16, 2024
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Corrected time stamps for ions and electrons.
Energy threshold shifts have been applied.
Changed EDB format, on-board anisotropies not possible in NM
Fill value inserted for J_p_lo__C4_PP_RAP: Noise
for time range 2024-09-30T12:06:32Z to 2024-09-30T12:06:37Z
Fill value inserted for J_p_hi__C4_PP_RAP: Noise
for time range 2024-09-30T12:06:32Z to 2024-09-30T12:06:37Z
 
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C4_PP_STA (spase://ESA/NumericalData/Cluster-Tango/STAFF/PrimeParameter/PT4S)
Description
N. Cornilleau et al,
The Cluster Spatio-Temporal Analysis of Field Fluctuations (Staff) Experiment
Space Sci. Rev., 79,  pp 107 - 136, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
PI Software Version 4.2, 25 September 2006
 
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C4_PP_WHI (spase://ESA/NumericalData/Cluster-Tango/WHISPER/PrimeParameter/PT4S)
Description
P. M. E. Decreau et al, WHISPER, A Resonance Sounder and Wave Analyser:
Performances and Perspectives for the Cluster Mission
Space Sci. Rev., 79,  pp 157 - 193, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
Two types of parameters are provided by WHISPER:
1) Density values (and quality): N_e_res and N_e_res_q, are related to sounding
operations.
The N_e_res value is calculated from an algorithm for resonance recognition,
which cannot take account of all level of information available to the
experimenter. The reliability of N_e_res parameters derived at the CSDS level
is thus limited in an unknown manner.
The N_e_res_q parameter (one value for each N_e_res data point) provides a crude
idea of the probability that the N_e_res value is actually correct. A value of
0 means that the value is probably wrong, a value above 80 that it is probably
correct. Anything in between reflects a crude evaluation of the chances. Refer
to PI for details.
2) Wave power values: E_pow_f4, E_pow_f5, E_pow_f6, E_pow_su and E_var_ts, are
related to recording of natural wave emissions.
Those parameters, not affected by variations in instrument's transfer functions,
are globally OK.
However, two factors can affect the precision of the measurements:
a) the occasional presence of spurious emissions created by operations of the
EDI instrument increases the wave power values measured on SC1, SC2 and SC3,
from an unknown amount,
b) the limited dynamical range of the instrument leads to an underestimation of
the E_pow parameters values when the voltage difference measured by the double
sphere antenna signal in the 2 - 80 kHz band is higher than 150 mVp or 600 mVp
(depending of the gain chosen). As a consequence, high values have to be taken
with special caution.
 
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C4_UP_FGM (spase://ESA/NumericalData/Cluster-Tango/FGM/UnvalidatedParameter/PT4S)
Description
A. Balogh et al, The Cluster Magnetic Field Investigation
Space Sci. Rev., 79,  pp 65 - 92, 1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Operational version of UKCDHF Pipeline software
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
*** C4_UP_FGM_20240930 HAS NOT BEEN VALIDATED - USE WITH CAUTION ***
For the extended mission (starting 1/1/2006) CSDS FGM products
are not validated prior to release to the science community.
Spikes and other artefacts that were previously removed during
validation of the FGM PP/SP data may occur in these files.
 
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C4_WAVEFORM_WBD doi:10.48322/nepa-q824
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bands in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'cluster_wbd_calibration.pdf'. Because the calibration was applied in the time
domain using a simple equation the raw counts actually measured by the WBD
instrument can be obtained by using these equations and solving for 'Raw
Counts', keeping in mind that this number is an Integer ranging from 0 to 255. 
Since DC offset is a real number, the resultant when solving for raw counts will
need to be converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, the
following steps need to be carried out:  1) If Electric Field, first divide
calibrated data by 1000 to get V m^-1; 2) Apply window of preference, if any
(such as Hanning, etc.); 3) Divide data values by sqrt(2) to get back to the rms
domain; 4) perform FFT (see Bandwidth variable notes for non-continuous modes);
5) divide by the noise bandwidth, which is equal to the sampling frequency
divided by the FFT size (see table below for appropriate sampling frequency); 6)
multiply by the appropriate constant for the window used, if any.
...
Bandwidth   Sample Rate
---------   ------------
9.5 kHz      27.443 kHz 
19 kHz       54.886 kHz 
77 kHz      219.544 kHz 
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Mar 2008.Revised Dec 2008, Jan 2010
 
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C4_WAVEFORM_WBD_BM2 (spase://NASA/NumericalData/Cluster-Tango/WBD/BM2/PT0.0000046S)
Description
High time resolution calibrated waveform data sampled in one of 3 frequency
bandwidths in the range 0-577 kHz along one axis using either an electric field
antenna or a magnetic search coil sensor.  The dataset also includes instrument
mode, data quality and the angles required to orient the measurement with
respect to the magnetic field and to the GSE coordinate system.
...
CALIBRATION:
...
The procedure used in computing the calibrated Electric Field and Magnetic Field
values found in this file can be obtained from the document
'CAA_EST_CR_WBD_v20.pdf'. Because the calibration was applied in the time domain
using a simple equation the raw counts actually measured by the WBD instrument
can be obtained by using these equations and solving for 'Raw Counts', keeping
in mind that this number is an Integer ranging from 0 to 255.  Since DC offset
is a real number, the resultant when solving for raw counts will need to be
converted to the nearest whole number.
...
CONVERSION TO FREQUENCY DOMAIN:
...
In order to convert the WBD data to the frequency domain via an FFT, see
'CAA_EST_CR_WBD_v20.pdf'. The steps for converting are briefly outlined below:
1) If Electric Field, first divide calibrated data by 1000 to get V m^-1; 2)
Apply window of preference, if any (such as Hanning, etc.); 3) Divide data
values by sqrt(2) to get back to the rms domain; 4) perform FFT (see Bandwidth
VAR_NOTES for non-continuous modes); 5) divide by the noise bandwidth, which is
equal to the sampling frequency divided by the FFT size (see table in VAR_NOTES
of the 'BM_Mode' variable for the appropriate sampling frequency); 6) multiply
by the appropriate constant for the window used, if any;7) if Translation is not
equal to 0, add the appropriate translation frequency to each frequency
component (see Translation CATDESC for the exact values).
...
COORDINATE SYSTEM USED:
...
One axis measurements made in the Antenna Coordinate System, i.e., if electric
field measurement, it will either be Ey or Ez, both of which are in the spin
plane of the spacecraft, and if magnetic field measurement, it will either be
Bx, along the spin axis, or By, in spin plane.
...
Modification History
Created Nov 2014.
 
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CASSINI_HELIO1DAY_POSITION doi:10.48322/7x96-1j49
Description
No TEXT global attribute value.
 
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CASSINI_HELIO1HR_POSITION doi:10.48322/7x96-1j49
Proper citations should include the "Accessed on date" in the form .
Description
No TEXT global attribute value.
 
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CASSINI_MAG_1MIN_MAGNETIC_FIELD doi:10.48322/vfsa-ej68
Description
Cassini magnetic-field 1 minute averages for the year 2020 in RTN  coordinates.
RTN coordinates consist of R (radial component, Sun tothe spacecraft), T
(tangential component, parallel to the Solar    Equatorial plane and
perpendicular to R), and N (normal component, completes right handed set).
This file contains a subset of all of the Cassini MAG data for 2001consisting of
only the data after the day of the last Jupiter      bowshock crossing
(2001-01-15).
This file was produced from raw (L1A) data at the PDS/PPI node usingsoftware
provided by the Cassini MAG team, and employing the latest calibration
available. The MAG team reports that while range-0 data are well calibrated,
higher range data needs improvement (see the   RANGE_CHANGES.ASC document for a
time history of range changes). Thesedata will be replaced as the calibration is
improved." 
The data are mostly from the fluxgate magnetometer (FGM). The tableat vhm.txt
identifies the 52 days in 2000-2004 for which the data are solely from the
vector helium magnetometer (VHM).  Days not in the table contain only FGM
data.VHM_mode variable indicates (value 1) whether data are from VHM
The data were produced from raw (L1A) data at the PDS/PPI node using software
provided by the Cassini MAG team, and employing the latest calibration
available.  PDS/PPI produced both 1-sec vectors and 1-min averages.  The MAG
team reports that while range-0 data are well calibrated for both FGM and VHM,
higher range data need improvement.  FGM_mode variable indicates (value 0) if
data is
range-0.Seehttp://www.igpp.ucla.edu/cgi-bin/ditdos?volume=COMAG_0XXX&folder=DOCU 
MENT/DATA_QUALITY&file=RANGE_CHANGESfor details.  In particular, this
documentation reports that FGM wasin range=0 for the following extended
intervals (plus other brief intervals):
1999/230/05 - 1999/245/07 (YYYY/DDD/HH, inclusive)1999/245/09 -
2000/037/122000/039/00 - 2000/053/182000/053/20 - 2000/056/012000/057/23 -
2002/334/132002/334/17 - 2003/292/182003/292/22 - 2004/046/112004/046/15 -
2004/088/082004/088/12 - 2004/136/062004/136/11 - 2004/174/012004/174/06 -
2004/182/17
 
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CIRBE_REPTILE-2_L1A_DETECTORS
Description
CIRBE is a 3U-CubeSat designed and developed by students and engineers at the
Laboratory for Atmospheric and Space Physics.
The primary objective of the science mission is to understand the formation of
the inner belt (L<2) electrons (100s of keV to multiple MeV), and to determine
the source, the intensity and dynamic variations of these electrons.
The goal is to make accurate measurements with fine energy resolution (>40
channels) for electrons of 0.3-3 MeV throughout the slot region and inner belt,
with secondary measurements of 6.7-35 MeV protons.
Such measurements are required to address the following science questions:
1) Where is the break point in terms of energy of electrons for a given event,
below which electrons can be transported into the inner belt from the outer belt
but above which electrons cannot, and what is the injection mechanism?
2) What is the CRAND contribution to inner belt electrons, and what is the low
energy neutron density near Earth?
3) What is the role of wave-particle interactions in shaping inner-belt electron
energy spectra?
A detailed description of the instrument can be found at
https://doi.org/10.1029/2021JA030249.
We acknowledge the use of the IRBEM library (4.4.0) to process the data, the
latest version of which can be found at .https://doi.org/10.5281/zenodo.6867552. 
 
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CIRBE_REPTILE-2_L1B_RNG_ELECS
Description
CIRBE is a 3U-CubeSat designed and developed by students and engineers at the
Laboratory for Atmospheric and Space Physics.
The primary objective of the science mission is to understand the formation of
the inner belt (L<2) electrons (100s of keV to multiple MeV), and to determine
the source, the intensity and dynamic variations of these electrons.
The goal is to make accurate measurements with fine energy resolution (>40
channels) for electrons of 0.3-3 MeV throughout the slot region and inner belt,
with secondary measurements of 6.7-35 MeV protons.
Such measurements are required to address the following science questions:
1) Where is the break point in terms of energy of electrons for a given event,
below which electrons can be transported into the inner belt from the outer belt
but above which electrons cannot, and what is the injection mechanism?
2) What is the CRAND contribution to inner belt electrons, and what is the low
energy neutron density near Earth?
3) What is the role of wave-particle interactions in shaping inner-belt electron
energy spectra?
A detailed description of the instrument can be found at
https://doi.org/10.1029/2021JA030249.
We acknowledge the use of the IRBEM library (4.4.0) to process the data, the
latest version of which can be found at .https://doi.org/10.5281/zenodo.6867552. 
 
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CIRBE_REPTILE-2_L2_RNG_ELECS
Description
CIRBE is a 3U-CubeSat designed and developed by students and engineers at the
Laboratory for Atmospheric and Space Physics.
The primary objective of the science mission is to understand the formation of
the inner belt (L<2) electrons (100s of keV to multiple MeV), and to determine
the source, the intensity and dynamic variations of these electrons.
The goal is to make accurate measurements with fine energy resolution (>40
channels) for electrons of 0.3-3 MeV throughout the slot region and inner belt,
with secondary measurements of 6.7-35 MeV protons.
Such measurements are required to address the following science questions:
1) Where is the break point in terms of energy of electrons for a given event,
below which electrons can be transported into the inner belt from the outer belt
but above which electrons cannot, and what is the injection mechanism?
2) What is the CRAND contribution to inner belt electrons, and what is the low
energy neutron density near Earth?
3) What is the role of wave-particle interactions in shaping inner-belt electron
energy spectra?
A detailed description of the instrument can be found at
https://doi.org/10.1029/2021JA030249.
We acknowledge the use of the IRBEM library (4.4.0) to process the data, the
latest version of which can be found at .https://doi.org/10.5281/zenodo.6867552. 
 
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CL_JP_PCY (spase://ESA/NumericalData/Cluster/JSOC/Predicted/SolarCycle/P1M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
New SILSO sunspot number series used for all records 
 in PCY files produced after 2 Aug 2015.
Caveats
JSOC predicted Solar cycle trends.
Please acknowledge sunspot numbers as:
Source: WDC-SILSO, Royal Observatory of Belgium, Brussels.
 
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CL_JP_PGP (spase://ESA/NumericalData/Cluster/Ephemeris/JP/PredictedGeometricPosition/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre,
 Space Sci. Rev. 79, 487-525 1997
For geometrical configuration parameters, p328 of Tetrahedron Geometric Factors
by P.Robert et al, in Analysis Methods for Multi-Spacecraft Data,
ed. G.Paschmann & P.Daly, pub. 1998 by the European Space Agency and
the International Space Institute, Bern.
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate dipole tilt and GSE-GSM 
 angle in PGP files produced after 23 Feb 2020.
Orbit number field supports 4-digit orbits and 6 figure phase 
 in PGP files produced after 20 March 2006.
Caveats
JSOC predicted Orbits.
 Using spacecraft C3 as reference spacecraft.
 
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CL_OR_GIFWALK
Description
Pre-generated ISTP orbit plots
 
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CL_SP_AUX (spase://ESA/NumericalData/Cluster/Ephemeris/SummaryParameter/PT60S)
Description
Orbital Parameters Calculated from Short Term Orbit File of RDM
For geometry configuration parameters, see p 328 of Tetrahedron Geometric
Factors
by P.Robert et al, in Analysis Methods for Multi-Spacecraft Data,
ed. G.Paschmann & P.Daly, pub. 1998 by the European Space Agency and
the International Space Institute, Bern.
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate
GSE-to-GSM angle and dipole tilt from 1 January 2020
Caveats
See CSDS User's Guide, DS-MPA-TN-0015, for post processing caveats
After C2 (Salsa) re-entry at 2024-09-08T18:47:36Z
auxiliary data provided for three spacecraft; use tetrahedron
geometry parameters, especially planarity values with caution
 
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CNOFS_CINDI_IVM_500MS doi:10.48322/r9x4-x639
Description
 The Communications/Navigation Outage Forecasting System (C/NOFS) is a prototype
operational system designed to monitor and forecast ionospheric scintillation in
real-time and on a global scale. In the space-borne segment, C/NOFS will fly a
system of proven sensors on-board a three-axis stabilized satellite to detect
ionospheric scintillation. This will provide data for global, real-time
specification, and 4 hour forecast capability.  
C/NOFS is a joint effort between the DOD Space Test Program and AFRL (Air Force
Research Laboratory). The space test program provides the spacecraft, launch
vehicle, launch and first year on-orbit operations.  AFRL is responsible for the
multi-instrument payload, payload integration  and test, model development, data
center operations, and product generation and distribution. 
The C/NOFS payload consists of six instruments: the Planar Langmuir Probe (PLP)
for measurements of plasma density, the Vector Electric Field Instrument (VEFI)
for measurements of vector electric and magnetic fields, the Ion Velocity Meter
(IVM) for measurements of plasma drift velocities and ion temperatures, the
Neutral Wind Meter (NWM) for measurements of neutral winds, the C/NOFS
Occultation Receiver for Ionospheric Sensing and Specification (CORISS) for
remote sensing of the electron density vertical profile, the Coherent
Electromagnetic Radio Tomography (CERTO) for measurements of ionospheric
scintillation parameters. Both the Neutral Wind Meter (NWM) and the Ion Velocity
Meter (IVM) are provided by NASA as the CINDI (Coupled Ion-Neutral Dynamics
Investigation) payload, which was selected as an Explorer Mission of
Opportunity.
 The goal of C/NOFS is to forecast scintillation three to six hours before its
onset such that system operators will be able to plan in ways that will optimize
mission command and control.
The spacecraft will be launched into an orbit with perigee/apogee of 400/700 km,
and an inclination of 13 degrees. Launch is currently planned for early 2006.
Information about C/NOFS can be found at Air Force Research Laboratory page:
http://www.kirtland.af.mil/shared/media/document/AFD-070404-094.pdf.
The Coupled Ion-Neutral Dynamics Investigation (CINDI) payload is funded by NASA
as an Explorer Mission of Opportunity. CINDI consists of two instruments: the
Ion Velocity Meter (IVM) and the Neutral Wind Meter (NWM). The IVM instrument
includes a ion drift meter and a retarding potential analyzer. IVM measure the
ion drift vector, the ion temperature, and the major ion composition with a
spatial resolution of about 4 km along the satellite track; the ion drift meter
also provides vertical and horizontal ion drift components at 500 m resolution.
The NWM consists of a cross track wind sensor and a ram wind sensor providing a
direct measure of the neutral wind vector with a spatial resolution of about 8
km along the satellite track.
 
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CNOFS_PLP_PLASMA_1SEC doi:10.48322/xnnr-w563
Description
The Planar Langmuir Probe on C/NOFS is a suite of 2 current measuring sensors
mounted on the ram facing surface of the spacecraft.  The primary sensor is an
Ion Trap (conceptually similar to RPAs flown on many other spacecraft) capable
of measuring ion densities as low as 1 cm-3 with a 12 bit log electrometer.  The
secondary senor is a swept bias planar Langmuir probe (Surface Probe) capable of
measuring Ne, Te, and spacecraft potential.
The ion number density is the one second average of the ion density sampled at
either 32, 256, 512, or 1024 Hz (depending on the mode).
The ion density standard deviation is the standard deviation of the samples used
to produce the one second average number density.
DeltaN/N is the detrened ion number density 1 second standard deviation divided
by the mean 1 sec density.
The electron density, electron temperature, and spacecraft potential are all
derived from a least squares fit to the current-bias curve from the Surface
Probe.
The data are PRELIMINARY, and as such, are intended for BROWSE PURPOSES ONLY.
Regestering your email will allow notification of updates.
 
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CNOFS_VEFI_BFIELD_1SEC doi:10.48322/vbt7-gj03
Description
The DC vector magnetometer on the CNOFS spacecraft is a three axis, fluxgate
sensor with active thermal control situated on a 0.6m boom.  This magnetometer
measures the Earth's magnetic field, B, using 16 bit A/D converters at 1 sample
per sec with a range of +/- 45,000 nT per sensor axis.  Its primary objective on
the CNOFS spacecraft is to enable the most accurate V x B and E x B measurements
along the spacecraft trajectory, where V is the spacecraft velocity in the fixed
frame of the earth and E is the ambient, measured electric field.  The magnetic
field data also provide indications of ionospheric currents as well as other
geophysical phenomena.  In-flight calibration of the raw magnetic field data is
carried out to determine gains, offsets, and the non-orthogonality matrix in the
sensor axes frame.   The IGRF-11 model is used as a reference to help determine
the calibration.  The calibrated magnetic field measurements are provided in the
data file.  A full description of the instrument can be found in the published
paper:  The Vector Electric Field Instrument (VEFI) on the C/NOFS Satellite,
Pfaff et al., 2021, doi.org/10.1007/s11214-021-00859-y.        
 
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CNOFS_VEFI_EFIELD_1SEC doi:10.48322/1dcn-xp86
Description
This data file contains information on the electric field solution as processed
by the VEFI team at NASA/Goddard Space Flight Center.  The data is PRELIMINARY,
and as such, is intended for BROWSE PURPOSES ONLY.  Registering your email will
allow notification of updates.
 
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CNOFS_VEFI_LD_500MS doi:10.48322/pv2n-aj92
Description
This data file contains the low rate data from the VEFI lightning detector. Two
photodiodes measure white light irradiance in 2 look directions and for 7
threshold values. Reference: Jacobson et al, J Atm Ocean Tech, 2011,
doi:10.1175/JTECH-D-11-00047.1
 
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CN_K0_ASI (spase://GBO/NumericalData/CANOPUS/ASI/KeyParameter/K0/PT1M)
Description
Images and intensities. 557.7nm Images binned to geodetic grid
References: 1.Rostoker, G., Samson, J.C., Creutzberg, F., Hughes, T.J.,
McDiarmid, D.R., McNamara, A.G., Vallance Jones, A., Wallis, D.D.,
Cogger, L.L.; CANOPUS - a ground based instrument array for remote sensing the 
high latitude ionosphere during the ISTP/GGS program, 
Space Sci. Rev., submitted for publication, 1993.
Modification History
Created 31-DEC-1999
 
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CN_K0_BARS (spase://GBO/NumericalData/CANOPUS/BARS/KeyParameter/K0/PT1M)
Description
North & East Velocity components at 336.5 EDFL long. from 64.2 to 67.0 EDFL lat.
References: 1.Rostoker, G., Samson, J.C., Creutzberg, F., Hughes, T.J.,
McDiarmid, D.R., McNamara, A.G., Vallance Jones, A., Wallis, D.D.,
Cogger, L.L.; CANOPUS - a ground based instrument array for remote sensing the 
high latitude ionosphere during the ISTP/GGS program, 
Space Sci. Rev., submitted for publication, 1993.
Modification History
Created  3-OCT-1994
 
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CN_K0_MARI (spase://GBO/NumericalData/CANOPUS/MARI/PT60S)
Description
Magnetic Field Extrema and Location
References: 1.Rostoker, G., Samson, J.C., Creutzberg, F., Hughes, T.J.,
McDiarmid, D.R., McNamara, A.G., Vallance Jones, A., Wallis, D.D.,
Cogger, L.L.; CANOPUS - a ground based instrument array for remote sensing the 
high latitude ionosphere during the ISTP/GGS program, 
Space Sci. Rev., submitted for publication, 1993.
Modification History
Created 31-DEC-1999
Added station Taloyoak on 29-SEP-1994
 
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CN_K0_MPA (spase://GBO/NumericalData/CANOPUS/MPA/KeyParameter/K0/PT1M)
Description
Station Status, Merged Scaled 5577A Scans and Peak Intensity
Merged Scans>from 3 stations along constant Geodetic Long. of 265, from Lat. 46
to 67
References: 1.Rostoker, G., Samson, J.C., Creutzberg, F., Hughes, T.J.,
McDiarmid, D.R., McNamara, A.G., Vallance Jones, A., Wallis, D.D.,
Cogger, L.L.; CANOPUS - a ground based instrument array for remote sensing the 
high latitude ionosphere during the ISTP/GGS program, 
Space Sci. Rev., submitted for publication, 1993.
2.Samson, J.C., Lyons, L.R., Newell, P.T., Creutzberg, F. and 
Xu, B., Proton aurora substorm intensifications, Geophys. Res. Letters,
19, 2167, 1992. 3.Samson, J.C., Hughes, T.J., Creutzberg, F., 
Wallis, D.D., Greenwald, R.A. and Ruohoniemi, J.M.,
Observations of a detached discrete arc in association with 
field line resonances, J. Geophys. Res., 96, 15, 683, 1991.
Modification History
Created 31-DEC-1999
 
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CN_K1_MARI (spase://GBO/NumericalData/CANOPUS/MARI/KeyParameter/K1/PT1M)
Description
Riometer measurements and Location
References: 1.Rostoker, G., Samson, J.C., Creutzberg, F., Hughes, T.J.,
McDiarmid, D.R., McNamara, A.G., Vallance Jones, A., Wallis, D.D.,
Cogger, L.L.; CANOPUS - a ground based instrument array for remote sensing the 
high latitude ionosphere during the ISTP/GGS program, 
Space Sci. Rev., submitted for publication, 1993.
Modification History
Created 31-DEC-1999
 
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COMETGS_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/GriggSkjellerup/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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COMETGS_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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COMETHMP_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/HondaMrkosPajdusakova/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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COMETHMP_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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CRRES_H0_MEA doi:10.48322/8e23-cz17
Description
CRRES MEA Data Archive
This is the re-processed version of the MEA data archive from the CRRES
spacecraft. 
The raw data provided by Principal Investigator A. Vampola have been processed
to derive 1 min average data. 
The data consists of counting rates from 17 energy channels in the range of
0.1-2 MeV and 19 pitch angle bins at 1 minute time intervals. 
The average flux, 90 degree flux and N value are included. 
Also included are the spacecraft geographic coordinates and altitude, L shell,
and the local and equatorial magnetic field magnitudes from the 1977
Olson-Pfitzer model of the earth's geomagnetic field.
The raw high resolution (0.512 sec) data and documentation of raw data can be
found at: https://spdf.gsfc.nasa.gov/pub/data/crres/particle_mea/ 
Modification History
Created May 2003
 
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CSSWE_REPTILE_6SEC-COUNTS-L1 doi:10.48322/dy3g-xz52
Description
CSSWE is a 3U-CubeSat designed and developed by students at the University of
Colorado at Boulder (CU-Boulder). The objective of the science mission is to
address fundamental questions pertaining to the relationship between solar
flares and energetic particles. These questions include the acceleration and
loss mechanisms of outer radiation belt electrons. 
The goal is to measure differential fluxes of relativistic electrons in the
energy range of 0.58-3.8 MeV and protons in 9-40 MeV. This project is a
collaborative effort between the Laboratory for Atmospheric and Space Physics
(LASP) and the Department of Aerospace Engineering Sciences (AES) at the
University of Colorado, which includes the participation of students, faculty,
and professional engineers. The science goals of the CSSWE mission are to study:
   How flare location, magnitude, and frequency relate to the timing, duration,
and energy spectrum of SEPs reaching Earth.
   How the energy spectrum of radiation belt electrons evolve and how this
evolution relates to the acceleration mechanism.
To accomplish these goals CSSWE has a requirement for a minimum of 3 months of
science operations based on expected flare and geomagnetic storm frequency. The
first month of operations will be utilized for systems stabilization and check
out.
 
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CSSWE_REPTILE_6SEC-FLUX-L2 doi:10.48322/brd0-ak96
Description
CSSWE is a 3U-CubeSat designed and developed by students at the University of
Colorado at Boulder (CU-Boulder). The objective of the science mission is to
address fundamental questions pertaining to the relationship between solar
flares and energetic particles. These questions include the acceleration and
loss mechanisms of outer radiation belt electrons. 
The goal is to measure differential fluxes of relativistic electrons in the
energy range of 0.58-3.8 MeV and protons in 9-40 MeV. This project is a
collaborative effort between the Laboratory for Atmospheric and Space Physics
(LASP) and the Department of Aerospace Engineering Sciences (AES) at the
University of Colorado, which includes the participation of students, faculty,
and professional engineers. The science goals of the CSSWE mission are to study:
   How flare location, magnitude, and frequency relate to the timing, duration,
and energy spectrum of SEPs reaching Earth.
   How the energy spectrum of radiation belt electrons evolve and how this
evolution relates to the acceleration mechanism.
To accomplish these goals CSSWE has a requirement for a minimum of 3 months of
science operations based on expected flare and geomagnetic storm frequency. The
first month of operations will be utilized for systems stabilization and check
out.
 
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CT_JP_PSE (spase://ESA/NumericalData/Cluster/Ephemeris/JP/PredictedScientificEvent/PT5M)
Description
M.A. Hapgood et al, The Joint Science Operations Centre, Space Sci. Rev. 79,
487-525 (1997)
NS S Southbound neutral sheet
NT I Enter north tail lobe from inner magnetosphere
ST O Leave south tail lobe for inner magnetosphere
Modification History
Produced in accordance with CSDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
IGRF 13th generation pole used to calculate GSM latitude and MLT 
 in PSE files produced after 23 Feb 2020.
PSE files updated to support orbits >999 and six decimal figures 
 on orbit phase from 25 March 2006.
Caveats
JSOC predicted scientific events.
 
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DAWN_HELIO1DAY_POSITION (spase://NASA/NumericalData/Dawn/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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DAWN_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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DE1_1MIN_RIMS doi:10.48322/4e3s-bm07
Description
The data were provided by Dennis Gallagher (MSFC). The Retarding Ion Mass
Spectrometer (RIMS) consisted of a retarding potential analyzer for energy
analysis in series with a magnetic ion-mass spectrometer for mass analysis.
Multiple sensor heads permitted the determination of the thermal plasma flow
characteristics. This instrument was designed to operate in two basic
commandable modes: a high-altitude mode in which the density, temperature, and
bulk-flow characteristics of principally H+, He+, and O+ ions were measured; and
a low-altitude mode that concentrated on the composition in the 1- to 32-u
range. This investigation provided information on (1) the densities of H+, He+,
and O+ ions in the ionosphere, plasmasphere, plasma trough, and polar cap
(including the density distribution along the magnetic vector in the vicinity of
the satellite apogee); (2) the temperature of H+, He+, and O+ ions in the
ionosphere, plasmasphere, plasma trough, and polar cap (energy range 0-45 eV);
(3) the bulk flow velocities of H+, He+, and O+ in the plasmapause, plasma
trough and polar cap; (4) the changing character of the cold plasma density,
temperature, and bulk flow in regions of interaction with hot plasma such as at
the boundary between the plasmasphere and the ring current; and (5) the detailed
composition of ionospheric plasma in the 1-to 32-u range. He++ and O++ were also
measured. The instrument consisted of three detector heads. One looked out in
the radial direction, and the other two were along the plus and minus spin-axis
directions. Each detector had a 55-deg half-cone acceptance angle. The detector
heads had a gridded, weakly collimating aperture where the retarding analysis
was performed, followed by a parallel plate ceramic magnetic mass analyzer with
two separate exit slits corresponding to ion masses in the ratio 1:4. Ions
exiting from these slits were detected with electron multipliers. In the apogee
mode, the thermal particle fluxes were measured while the potential on a set of
retarding grids was stepped through a sequence of settings. In the perigee mode,
the retarding grids were grounded and the detector utilized a continuous
acceleration potential sweep that focused the mass ranges from 1 to 8, and 4 to
32 u. Time resolution was 16 msec. Additional details can be found in C. R.
Chappell et al., Space Sci. Instrum., v. 5, n. 4, p. 477, 1981.
Criterian for selecting data points to be fitted aperature bias = 0 must have at
least 10 or more non-zero points in rpa curve.  if less that 1.3 Re high voltage
monitor must be turned on maximum countr rate value must at least 5.0 must have
at least 4 points starting from end of rpa curve find 3 consecutive point of
increasing value, reset end of rpa curve to here make certain last point is 1
sigma above noise level (the points excluded in previous step), if not drop
point and check new last point, continue until criteria is met, must have at
least 3 points left starting at new end of selected rpa curve stop first point
greater that 80% of maximum of spin curve, if non found stop at last point less
that maximum, must have at least 3 points left change curve from count rate
curve to l**2 curve if number of points are 5 or less: do a linear least squares
fit (linfit) to the data, if the linear correlation coefficient (lcc) greater
than 0.800 then points will be used, if not, data set is discarded if number of
points are greater then 5: do a linfit to the bottom 5 and a linfit to the top 5
points, in 6 or more points do linfit to the middle 5, saving the lcc and slope
for each case. if all three lccs are less than 0.800 discard data set through a
series of tests find the set of 5 with the best lcc slope combination once set
of 5 has been selected add rest of points one at a time and redo linfit, if lcc
gets worse discard point otherwise keep it, do this until all points are checked
we now have the points to be used
Two Dynamics Explorer (DE) spacecraft were launched August 3, 1981, and placed
into coplanar polar orbits with DE-1 in a highly elliptical orbit and DE-2 in a
lower more circular orbit. The primary objective of the DE program was to
investigate magnetosphere-ionosphere-atmosphere coupling processes.
The DE mission provided a wealth of new information on a wide variety of
magnetospheric plasma wave phenomena including auroral kilometric radiation,
auroral hiss, Z mode radiation, narrow-band electromagnetic emissions associated
with equatorial upper hybrid waves, whistler mode emissions, wave-particle
interactions stimulated by ground VLF transmitters, equatorial ion
cyclotron.emissions, ion Bernstein mode emissions, and electric field turbulence
along the auroral field lines. 
 
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DE1_2SEC_OA
Description
Dynamics Explorer 1 spacecraft was one of two satellites in the Dynamics
Explorer program.  The DE-1 and DE-2 satellites were launched by the same
vehicle so that their orbits would be coplanar, allowing two-point measurements
along magnetic field lines, for the purpose of studying coupling between the
magnetosphere, ionosphere, and upper atmosphere.  The DE-1 orbit was highly
elliptical with an apogee of 4.35 Re and a perigee of 500 km whereas the DE-2
spacecraft was placed in a much lower 300 x 1000 km altitude orbit. DE-1 was
spin stabilized with its spin axis normal to the plane of the orbit. DE-2 was
three axis stabilized with one face being nadir oriented. 
The study of field-aligned currents and MHD waves were the primary objectives of
the DE-1/2 magnetometer investigation. Comparison of the magnetometer data with
measurements of precipitating charged particles yielded new information on the
field-aligned current carriers.  In combination with the electric field
measurements, it was possible to determine the vertical Poynting Flux of
electromagnetic energy flowing between the magnetosphere and ionosphere and to
separate small-scale field-aligned currents from MHD waves through the
evaluation of the local ratio of the electric to magnetic field amplitudes in
these perturbations. The field-aligned current measurements and neutral
atmosphere observations also provided an opportunity for investigating
atmosphere-magnetosphere coupling and assessing the total rate of energy
transfer into the upper atmosphere.  Finally, the DE-1/2 magnetometer
investigation provided a vital service in so far as a knowledge of magnetic
field direction and intensity is essential to any number of space plasma science
investigations utilizing the various DE-1/2 particles and fields data sets. 
The DE-1 magnetic field (MAG-A) 6-second average resolution data set consists of
averages of the high resolution triaxial fluxgate measurements taken every 62.5
msec (i.e., 16 vectors/second).  The MAG-A data set consists of the three
components of the model magnetic field and difference field, B-Radial (Br),
B-Theta (Bth), and B-Phi (Bph), in *old* Geomagnetic Spherical (GMS)
Coordinates, and the difference field in local *new* Geographic Spherical (GGS)
and Geomagnetic Spherical (GMS) Coordinates, respectively, and the difference
field in local magnetic coordinates (b-para, b-parp1, b-parp2).  The R, Theta
and Phi axes are positive in the directions of increasing radial distance from
the center of the Earth (i.e., outward), increasing magnetic colatitude (i.e.,
southward) and increasing azimuth angle (i.e., magnetic east). The reference for
the MAGSAT magnetic field model is Langel et al., Geophys. Res. Lett., 7, 793,
1980. The following Orbit Attitude (OA) parameters are also included in the data
set: altitude, geographic latitude and longitude, magnetic local time, and
invariant latitude. The data are provided in daily files in ASCII format.
[updated by Robert.M.Candey@nasa.gov, 2006 Jan 17, per email dated Date: Thu, 18
Feb 99 17:08:59 JST From: iyemori@swdcgw.kugi.kyoto-u.ac.jp (Toshihiko_Iyemori)]
As described in Farthing et al. (1981), the DE-1 magnetometer had a digital
resolution of +1.5 nT in its low altitude, least sensitive mode. Two higher
sensitivity modes were used at higher altitudes with digital resolutions of
+0.25 nT and +0.02 nT, respectively. The data set consists of daily files from
81258 to 91049 in ASCII format. Each file contains all of the data available for
a given day.
The dominant source of error in the DE-1 magnetic field measurements is the
uncertainty in the attitude of the spacecraft. The DE-1 spacecraft was designed
to an attitude uncertainty specification of about 0.3 degree which appears to
have been met much of the time. As a rule of thumb each 0.1 degree in attitude
uncertainty near perigee corresponds to an error of approximately 100 nT in each
component of the field when the magnetic field measured at the sensors is
transferred to an inertial frame of reference or a model field is transferred
into the 0spacecraft frame and subtracted from the measured field.  For this
reason it is common for the residual, or delta-B field obtained by subtracting
the model field at low altitudes (i.e., high fields) to show a gradual shift of
several 100 nT from the start of a passage across the polar cap to the other
side.  (These slow shifts in the baselines of the vector field components do not
affect most scientific analyses, e.g., field-aligned current measurements, but
they can be effectively dealt with through modeling if need be.  At higher
altitudes the ambient field intensity is less and the uncertainty due to
attitude errors is correspondingly smaller.
The absolute accuracy of the DE-1 total magnetic field measurement has also been
evaluated through comparison with the precision vector/scalar magnetic field
observatories located on the ground which are used to monitor the geomagnetic
field. On the basis of such cross-comparisons utilizing DE-1 perigee data over
the life of the mission, R. Langel (private communication, 1994) found excellent
agreement between the MAG-A and ground-based observatory scalar data sets at the
20 to 40 nT level. 
In using any unfamiliar data set, caution is advised and tests to screen out
instrumental artifacts should be devised before reaching important conclusions.
De-spinning high sensitivity, boom mounted vector magnetometer data in high
fields (i.e., >1000 nT) frequently results in a readily observable residual
signal at the spin period and its harmonics. In the case of the DE-1
magnetometer measurements, the dominant causes of residual spin tone were found
to be small (0.1 to 0.01%) changes in the instrument scale factors and boom
bending of up to several tenths of a degree in response to varying thermal
inputs due to orbit/attitude driven changes in solar illumination (e.g.,
seasonal variations, eclipses, etc.). These effects were minimized through an
orbit by orbit calibration procedure which analyzed the residual spin tone
around apogee and perigee and adjusted the scale factors and sensor attitude
accordingly. Even after these in-flight calibration activities, residual spin
tone signals in the MAG-A data with amplitudes of tens of nanotesla are common
in high fields around perigee. The most probable cause of these residuals is the
transverse field dependence of fluxgate magnetometers in high fields which was
not well-appreciated at the time that DE-1/2 magnetometers were designed and
calibrated in the late 1970's. As discussed by Luhr et al. (1995) in regards to
the magnetometer on the low altitude, spin stabilized Freja spacecraft, this
non-linear effect can easily produce the residual spin frequency signals present
in the MAG-A data set. 
The MLT and ILAT algorithms were supplied by M. Sugiura (PI for the Magnetometer
Investigation) prior to launch and used in the generation of the Orbit-Attitude
database.
References:               
1. The Instrument Data File Set. URL http://pemrac.space.swri.edu/spds/data.html 
Modification History
Initial Release
 
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DE1_62MS_MAGA-GMS
Description
Dynamics Explorer 1 spacecraft was one of two satellites in the Dynamics
Explorer program.  The DE-1 and DE-2 satellites were launched by the same
vehicle so that their orbits would be coplanar, allowing two-point measurements
along magnetic field lines, for the purpose of studying coupling between the
magnetosphere, ionosphere, and upper atmosphere.  The DE-1 orbit was highly
elliptical with an apogee of 4.35 Re and a perigee of 500 km whereas the DE-2
spacecraft was placed in a much lower 300 x 1000 km altitude orbit. DE-1 was
spin stabilized with its spin axis normal to the plane of the orbit. DE-2 was
three axis stabilized with one face being nadir oriented. 
The study of field-aligned currents and MHD waves were the primary objectives of
the DE-1/2 magnetometer investigation. Comparison of the magnetometer data with
measurements of precipitating charged particles yielded new information on the
field-aligned current carriers.  In combination with the electric field
measurements, it was possible to determine the vertical Poynting Flux of
electromagnetic energy flowing between the magnetosphere and ionosphere and to
separate small-scale field-aligned currents from MHD waves through the
evaluation of the local ratio of the electric to magnetic field amplitudes in
these perturbations. The field-aligned current measurements and neutral
atmosphere observations also provided an opportunity for investigating
atmosphere-magnetosphere coupling and assessing the total rate of energy
transfer into the upper atmosphere.  Finally, the DE-1/2 magnetometer
investigation provided a vital service in so far as a knowledge of magnetic
field direction and intensity is essential to any number of space plasma science
investigations utilizing the various DE-1/2 particles and fields data sets.  
The DE-1 magnetic field (MAG-A) high time resolution data set consists of
triaxial fluxgate measurements taken every 62.5 msec (i.e., 16 vectors/second). 
As described in Farthing et al. (1981), the DE-1 magnetometer had a digital
resolution of +1.5 nT in its low altitude, least sensitive mode. Two higher
sensitivity modes were used at higher altitudes with digital resolutions of
+0.25 nT and +0.02 nT, respectively. The MAG-A data set consists of the three
components of the magnetic field, B-Radial (Br), B-Theta (Bth), and B-Phi (Bph),
in Geomagnetic Spherical (GMS) Coordinates. This is a local Cartesian coordinate
system. The R, Theta and Phi axes are oriented relative to a MAGSAT magnetic
field model (Langel et al., 1980) positive in the directions of increasing
radial distance from the center of the Earth (i.e., outward), increasing
magnetic colatitude (i.e., southward) and increasing azimuth angle (i.e.,
magnetic east). The following Orbit Attitude (OA) parameters are also included
in the archive data set: model magnetic field in GMS coordinates; altitude of
the satellite; magnetic latitude and longitude; magnetic local time, and
invariant latitude. The data set consists of daily files from 81258 to 91049.
Each file contains all of the data available for a given day. If there were no
magnetometer data for a given time, the time record was left out. If there were
magnetometer data, but no orbit or model field data, a fill value of 9999999.0
was used for the missing values.  
The dominant source of error in the DE-1 magnetic field measurements is the
uncertainty in the attitude of the spacecraft. The DE-1 spacecraft was designed
to an attitude uncertainty specification of about 0.3 degree which appears to
have been met much of the time. As a rule of thumb each 0.1 degree in attitude
uncertainty near perigee corresponds to an error of approximately 100 nT in each
component of the field when the magnetic field measured at the sensors is
transferred to an inertial frame of reference or a model field is transferred
into the 0spacecraft frame and subtracted from the measured field.  For this
reason it is common for the residual, or delta-B field obtained by subtracting
the model field at low altitudes (i.e., high fields) to show a gradual shift of
several 100 nT from the start of a passage across the polar cap to the other
side.  (These slow shifts in the baselines of the vector field components do not
affect most scientific analyses, e.g., field-aligned current measurements, but
they can be effectively dealt with through modeling if need be.  At higher
altitudes the ambient field intensity is less and the uncertainty due to
attitude errors is correspondingly smaller.
The absolute accuracy of the DE-1 total magnetic field measurement has also been
evaluated through comparison with the precision vector/scalar magnetic field
observatories located on the ground which are used to monitor the geomagnetic
field. On the basis of such cross-comparisons utilizing DE-1 perigee data over
the life of the mission, R. Langel (private communication, 1994) found excellent
agreement between the MAG-A and ground-based observatory scalar data sets at the
20 to 40 nT level. 
On time scales comparable to or less than the DE-1 spin period, 6 sec, other
artifacts are present in the data set which must be considered for
somescientific investigations. Like most telemetered geophysical data, the
vector.components archived here suffer from occasional bad data points. These
spurious data entries were caused, for the most part, by noise introduced in the
satellite-receiving station telemetry link. Such bad data can usually be
recognized by workers familiar with such data sets. These are for the most part
single point data excursions which show no geophysical correlation between the
magnetic field components and the observations of plasma phenomena by the other
DE instruments. Similarly, there sometimes exist spurious data points in the
ancillary orbit/attitude database.  Some are obvious such as model magnetic
field values for which the sign values have been corrupted. Others, such as
occasional millisecond jumps in the time, produce small, unphysical
discontinuities in the processed field components. Small discontinuities are
also sometimes present at the point where the magnetometer changes mode due to
slight imperfections in calibration parameters which are independently
determined for each mode. (N.B., mode changes can be readily detected by the
change in the digital resolution of the data in an expanded vertical scale plot
of B versus time.) In using any unfamiliar data set, caution is advised and
tests to screen out instrumental artifacts should be devised before reaching
important conclusions.
De-spinning high sensitivity, boom mounted vector magnetometer data in high
fields (i.e., >1000 nT) frequently results in a readily observable residual
signal at the spin period and its harmonics. In the case of the DE-1
magnetometer measurements, the dominant causes of residual spin tone were found
to be small (0.1 to 0.01%) changes in the instrument scale factors and boom
bending of up to several tenths of a degree in response to varying thermal
inputs due to orbit/attitude driven changes in solar illumination (e.g.,
seasonal variations, eclipses, etc.). These effects were minimized through an
orbit by orbit calibration procedure which analyzed the residual spin tone
around apogee and perigee and adjusted the scale factors and sensor attitude
accordingly. Even after these in-flight calibration activities, residual spin
tone signals in the MAG-A data with amplitudes of tens of nanotesla are common
in high fields around perigee. The most probable cause of these residuals is the
transverse field dependence of fluxgate magnetometers in high fields which was
not well-appreciated at the time that DE-1/2 magnetometers were designed.and
calibrated in the late 1970's. As discussed by Luhr et al. (1995) in regards to
the magnetometer on the low altitude, spin stabilized Freja spacecraft, this
non-linear effect can easily produce the residual spin frequency signals present
in the MAG-A data set.
 
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DE1_6SEC_MAGAGMS doi:10.48322/ps14-8x77
Description
Dynamics Explorer 1 spacecraft was one of two satellites in the Dynamics
Explorer program.  The DE-1 and DE-2 satellites were launched by the same
vehicle so that their orbits would be coplanar, allowing two-point measurements
along magnetic field lines, for the purpose of studying coupling between the
magnetosphere, ionosphere, and upper atmosphere.  The DE-1 orbit was highly
elliptical with an apogee of 4.35 Re and a perigee of 500 km whereas the DE-2
spacecraft was placed in a much lower 300 x 1000 km altitude orbit. DE-1 was
spin stabilized with its spin axis normal to the plane of the orbit. DE-2 was
three axis stabilized with one face being nadir oriented. 
The study of field-aligned currents and MHD waves were the primary objectives of
the DE-1/2 magnetometer investigation. Comparison of the magnetometer data with
measurements of precipitating charged particles yielded new information on the
field-aligned current carriers.  In combination with the electric field
measurements, it was possible to determine the vertical Poynting Flux of
electromagnetic energy flowing between the magnetosphere and ionosphere and to
separate small-scale field-aligned currents from MHD waves through the
evaluation of the local ratio of the electric to magnetic field amplitudes in
these perturbations. The field-aligned current measurements and neutral
atmosphere observations also provided an opportunity for investigating
atmosphere-magnetosphere coupling and assessing the total rate of energy
transfer into the upper atmosphere.  Finally, the DE-1/2 magnetometer
investigation provided a vital service in so far as a knowledge of magnetic
field direction and intensity is essential to any number of space plasma science
investigations utilizing the various DE-1/2 particles and fields data sets. 
The DE-1 magnetic field (MAG-A) 6-second average resolution data set consists of
averages of the high resolution triaxial fluxgate measurements taken every 62.5
msec (i.e., 16 vectors/second).  The MAG-A data set consists of the three
components of the model magnetic field and difference field, B-Radial (Br),
B-Theta (Bth), and B-Phi (Bph), in *old* Geomagnetic Spherical (GMS)
Coordinates, and the difference field in local *new* Geographic Spherical (GGS)
and Geomagnetic Spherical (GMS) Coordinates, respectively, and the difference
field in local magnetic coordinates (b-para, b-parp1, b-parp2).  The R, Theta
and Phi axes are positive in the directions of increasing radial distance from
the center of the Earth (i.e., outward), increasing magnetic colatitude (i.e.,
southward) and increasing azimuth angle (i.e., magnetic east). The reference for
the MAGSAT magnetic field model is Langel et al., Geophys. Res. Lett., 7, 793,
1980. The following Orbit Attitude (OA) parameters are also included in the data
set: altitude, geographic latitude and longitude, magnetic local time, and
invariant latitude. The data are provided in daily files in ASCII format.
[updated by Robert.M.Candey@nasa.gov, 2006 Jan 17, per email dated Date: Thu, 18
Feb 99 17:08:59 JST From: iyemori@swdcgw.kugi.kyoto-u.ac.jp (Toshihiko_Iyemori)]
As described in Farthing et al. (1981), the DE-1 magnetometer had a digital
resolution of +1.5 nT in its low altitude, least sensitive mode. Two higher
sensitivity modes were used at higher altitudes with digital resolutions of
+0.25 nT and +0.02 nT, respectively. The data set consists of daily files from
81258 to 91049 in ASCII format. Each file contains all of the data available for
a given day. 
The dominant source of error in the DE-1 magnetic field measurements is the
uncertainty in the attitude of the spacecraft. The DE-1 spacecraft was designed
to an attitude uncertainty specification of about 0.3 degree which appears to
have been met much of the time. As a rule of thumb each 0.1 degree in attitude
uncertainty near perigee corresponds to an error of approximately 100 nT in each
component of the field when the magnetic field measured at the sensors is
transferred to an inertial frame of reference or a model field is transferred
into the 0spacecraft frame and subtracted from the measured field.  For this
reason it is common for the residual, or delta-B field obtained by subtracting
the model field at low altitudes (i.e., high fields) to show a gradual shift of
several 100 nT from the start of a passage across the polar cap to the other
side.  (These slow shifts in the baselines of the vector field components do not
affect most scientific analyses, e.g., field-aligned current measurements, but
they can be effectively dealt with through modeling if need be.  At higher
altitudes the ambient field intensity is less and the uncertainty due to
attitude errors is correspondingly smaller.
The absolute accuracy of the DE-1 total magnetic field measurement has also been
evaluated through comparison with the precision vector/scalar magnetic field
observatories located on the ground which are used to monitor the geomagnetic
field. On the basis of such cross-comparisons utilizing DE-1 perigee data over
the life of the mission, R. Langel (private communication, 1994) found excellent
agreement between the MAG-A and ground-based observatory scalar data sets at the
20 to 40 nT level. 
In using any unfamiliar data set, caution is advised and tests to screen out
instrumental artifacts should be devised before reaching important conclusions.
De-spinning high sensitivity, boom mounted vector magnetometer data in high
fields (i.e., >1000 nT) frequently results in a readily observable residual
signal at the spin period and its harmonics. In the case of the DE-1
magnetometer measurements, the dominant causes of residual spin tone were found
to be small (0.1 to 0.01%) changes in the instrument scale factors and boom
bending of up to several tenths of a degree in response to varying thermal
inputs due to orbit/attitude driven changes in solar illumination (e.g.,
seasonal variations, eclipses, etc.). These effects were minimized through an
orbit by orbit calibration procedure which analyzed the residual spin tone
around apogee and perigee and adjusted the scale factors and sensor attitude
accordingly. Even after these in-flight calibration activities, residual spin
tone signals in the MAG-A data with amplitudes of tens of nanotesla are common
in high fields around perigee. The most probable cause of these residuals is the
transverse field dependence of fluxgate magnetometers in high fields which was
not well-appreciated at the time that DE-1/2 magnetometers were designed and
calibrated in the late 1970's. As discussed by Luhr et al. (1995) in regards to
the magnetometer on the low altitude, spin stabilized Freja spacecraft, this
non-linear effect can easily produce the residual spin frequency signals present
in the MAG-A data set. 
The MLT and ILAT algorithms were supplied by M. Sugiura (PI for the Magnetometer
Investigation) prior to launch and used in the generation of the Orbit-Attitude
database.
 
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DE1_PWI_LFC-SPECTRA doi:10.48322/hx4p-3v35
Description
S. D. Shawhan, D. A. Gurnett, D. L. Odem, R. A. Helliwell, and C. G. Park, The
plasma wave and quasi-static electric field instrument (PWI) for Dynamics
Explorer-A, Space Sci. Instrumen., 5, 535, 1981.
Two Dynamics Explorer (DE) spacecraft were launched August 3, 1981, and placed
into coplanar polar orbits with DE-1 in a highly elliptical orbit and DE-2 in a
lower more circular orbit. The primary objective of the DE program was to
investigate magnetosphere-ionosphere-atmosphere coupling processes.
The DE mission provided a wealth of new information on a wide variety of
magnetospheric plasma wave phenomena including auroral kilometric radiation,
auroral hiss, Z mode radiation, narrow-band electromagnetic emissions associated
with equatorial upper hybrid waves, whistler mode emissions, wave-particle
interactions stimulated by ground VLF transmitters, equatorial ion cyclotron
emissions, ion Bernstein mode emissions, and electric field turbulence along the
auroral field lines. 
This file contains calibrated, full resolution, data from the DE-1 Plasma Wave
Instrument (PWI).  This instrument was designed and built by the plasma wave
group at The University of Iowa, Department of Physics and Astronomy, in
collaboration with investigators at Stanford University's STAR Laboratory.  It
measured plasma wave phenomena and quasi-static electric fields using paired
combinations of five PWI sensors: a 200m tip-to-tip long wire electric antenna
deployed in the spacecraft spin plane, a 9m tip-to-tip tubular electric antenna
deployed along the spacecraft spin axis, a short 0.6m electric antenna, mounted
on the boom and oriented parallel to the long wire antenna, a magnetic loop
antenna mounted on the boom and oriented to measure the component of the
magnetic field parallel to the long wire antenna, and a magnetic search coil
antenna, also mounted on a boom and oriented to measure the magnetic field
parallel to the spacecraft spin axis.
The PWI main electronics unit consisted of a Step Frequency Correlator (SFC), a
Low Frequency Correlator (LFC), a Wideband Analog Receiver (WBR) and a Linear
Wave Receiver (LWR).  Only the LFC data are included in these files.  The SFC
data were provided in a companion fileset.  A dataset containing available high
rate WBR LWR data may be provided in future archive products.
The LFC consisted of two receivers (LFR-A and LFR-B) with 8 analog channels
each. The analog channels were centered at 1.78, 3.12, 5.62, 10.0, 17.8, 31.2,
56.2 and 100 Hz.  Each channel's band-edge was at +/-15% of the center value. 
Each LFR in the LFC could be connected to either the Ex, Es, Ez, or H antenna
during an 8 second major frame.  In addition, the Low Frequency Correlator
provided in-phase and quadrature-phase correlations of signals from any selected
antenna pair.  Phase data are not provided in this file set.
For a detailed description of the Plasma Wave Instrument, the reader is referred
to the Space Science Instrumentation referenece above.
 
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DE1_PWI_OR-AT doi:10.48322/wma0-gq05
Description
S. D. Shawhan, D. A. Gurnett, D. L. Odem, R. A. Helliwell, and C. G. Park, The
plasma wave and quasi-static electric field instrument (PWI) for Dynamics
Explorer-A, Space Sci. Instrumen., 5, 535, 1981.
Two Dynamics Explorer (DE) spacecraft were launched August 3, 1981, and placed
into coplanar polar orbits with DE-1 in a highly elliptical orbit and DE-2 in a
lower more circular orbit. The primary objective of the DE program was to
investigate magnetosphere-ionosphere-atmosphere coupling processes.
The DE mission provided a wealth of new information on a wide variety of
magnetospheric plasma wave phenomena including auroral kilometric radiation,
auroral hiss, Z mode radiation, narrow-band electromagnetic emissions associated
with equatorial upper hybrid waves, whistler mode emissions, wave-particle
interactions stimulated by ground VLF transmitters, equatorial ion cyclotron
emissions, ion Bernstein mode emissions, and electric field turbulence along the
auroral field lines. 
This file contains 8 second resolution emphemeris and spacecraft attitude
parameters that coincide with DE-1 telemetry frames containing PWI lowrate data.
 These parameters are not to be taken as an authoritative set, but are
convenient when working with PWI science data products.  Most of these data are
provided in the Geocentric Equatorial Inertial (GEI) TOD reference frame.  The Z
axis of the GEI frame is parallel to Earth's spin axis; the X axis points
towards the First Point of Aries with the Y axis aligned so as to generate a
right-handed coordinate system.
For a detailed description of the Plasma Wave Instrument, the reader is referred
to the Space Science Instrumentation referenece above.
 
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DE1_PWI_SFC-SPECTRA doi:10.48322/cb14-a164
Description
S. D. Shawhan, D. A. Gurnett, D. L. Odem, R. A. Helliwell, and C. G. Park, The
plasma wave and quasi-static electric field instrument (PWI) for Dynamics
Explorer-A, Space Sci. Instrumen., 5, 535, 1981.
Two Dynamics Explorer (DE) spacecraft were launched August 3, 1981, and placed
into coplanar polar orbits with DE-1 in a highly elliptical orbit and DE-2 in a
lower more circular orbit. The primary objective of the DE program was to
investigate magnetosphere-ionosphere-atmosphere coupling processes.
The DE mission provided a wealth of new information on a wide variety of
magnetospheric plasma wave phenomena including auroral kilometric radiation,
auroral hiss, Z mode radiation, narrow-band electromagnetic emissions associated
with equatorial upper hybrid waves, whistler mode emissions, wave-particle
interactions stimulated by ground VLF transmitters, equatorial ion
cyclotron.emissions, ion Bernstein mode emissions, and electric field turbulence
along the auroral field lines. 
This file contains calibrated, full resolution, data from the DE-1 Plasma Wave
Instrument (PWI).  This instrument was designed and built by the plasma wave
group at The University of Iowa, Department of Physics and Astronomy, in
collaboration with investigators at Stanford University's STAR Laboratory.  It
measured plasma wave phenomena and quasi-static electric fields using paired
combinations of five PWI sensors: a 200m tip-to-tip long wire electric antenna
deployed in the spacecraft spin plane, a 9m tip-to-tip tubular electric antenna
deployed along the spacecraft spin axis, a short 0.6m electric antenna, mounted
on the boom and oriented parallel to the long wire antenna, a magnetic loop
antenna mounted on the boom and oriented to measure the component of the
magnetic field parallel to the long wire antenna, and a magnetic search coil
antenna, also mounted on a boom and oriented to measure the magnetic field
parallel to the spacecraft spin axis.
The PWI main electronics unit consisted of a Step Frequency Correlator (SFC), a
Low Frequency Correlator (LFC), a Wideband Analog Receiver (WBR) and a Linear
Wave Receiver (LWR).  Only the SFC data are included in these files.  The LFC
data were provided in a companion fileset.  A dataset containing available high
rate WBR LWR data may be provided in the future.
The SFC consisted of two Step Frequency Receivers (SFR-A and SFR-B) which
provided amplitude  measurements of the electric and magnetic fields from 100 Hz
to 400 kHz and in-phase and quadrature-phase correlations of signals from any
selected antenna pair.  Phase data are not provided in this file set.
For a detailed description of the Plasma Wave Instrument, the reader is referred
to the Space Science Instrumentation referenece above.
 
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DE2_62MS_VEFIMAGB doi:10.48322/ha70-4305
Description
This data set is a combination of the VEFI and MAGB high resolution data sets in
SPC coordinates submitted to NSSDC.  The following OA parameters have been added
to the data set:  Model magnetic field in SPC coordinates, altitude of the
satellite, geographic latitude and longitude, magnetic local time, and invariant
latitude.  The VEFI data set is described in the file VEFIVOLDESC.SFD and the
MAGB data set is described in the file MAGBVOLDESC.SFD, these files are portions
of the SFDU metadata files submitted with the VEFI and MAGB data to NSSDC and
are included in each volume of this data set.  This data set consists of daily
files from day 81227 to day 83047.  Each file contains all the data available
for a given day.  During the merging of the data sets it was found that although
VEFI and MAGB should cover the same time spans, they do not, due perhaps to the
fact that the original MAGB high resolution data set was created on the DE
Sigma-9 using the DE telemetry tapes, while the VEFI high resolution data set
was created on the DE MicroVAX system using the DE telemetry data base on
optical disk.  In order to keep the largest amount of data possible, the merged
data set includes all the available VEFI and MAGB data, for those times when
VEFI data was available but MAGB was not (6.54%), a fill data value of 9999999.
was given to the MAGB data and for those times when MAGB data was available but
VEFI was not (6.87%), the fill data value was assigned to the VEFI data.  Times
for which both VEFI and MAGB data were fill values in the original data sets
were not included in the merged data set.  There were also times when certain OA
parameters were fill values in the OA data base and they are therefore also fill
values in this merged data set.  The model magnetic field had fill values for
8.55% of the data.  Statistics were not kept for the other OA parameters.  Each
daily file contains a record per measurement.  The total number of records in
each file varies depending on the amount of data available for a given day. 
Each record of each daily file contains the following information:
 
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DE2_AC500MS_VEFI doi:10.48322/x1km-9q17
Proper citations should include the "Accessed on date" in the form .
Description
The Vector Electric Field Instrument (VEFI) used flight-proven double-probe
techniques with 20-m baselines to obtain measurements of dc electric fields.
This electric field investigation had the following objectives: (1) to obtain
accurate and comprehensive triaxial dc electric field measurements at
ionospheric altitudes in order to refine the basic spatial patterns, define the
large-scale time history of these patterns, and study the small-scale temporal
and spatial variations within the overall patterns; (2) to study the degree to
which and in what region the electric field projects to the equatorial plane;
(3) to obtain measurements of extreme low frequency (ELF) and lower frequency
irregularity structures; and (4) to perform numerous correlative studies. The
instrument consisted of six cylindrical elements 11 m long and 28 mm in
diameter. Each antenna was insulated from the plasma except for the outer 2 m.
The baseline, or distance between the midpoints of these 2-m active elements,
was 20 m. The antennas were interlocked along the edges to prevent oscillation
and to increase their rigidity against drag forces. The basic electronic system
was very similar in concept to those used on IMP-J and ISEE 1, but modified for
a three-axis measurement on a nonspinning spacecraft. At the core of the system
were the high-impedance (1.E12 ohm) preamplifiers, whose outputs were accurately
subtracted and digitized (14-bit A/D conversion for sensitivity to about 0.1
microvolt/m) to maintain high resolution, for subsequent removal of the
cross-product of the vectors V and B in data processing. This provided the basic
dc measurement. Other circuitry was used to aid in interpreting the dc data and
to measure rapid variations in the signals detected by the antennas. The planned
dc electric field range was plus or minus 1 V/m, the planned resolution was 0.1
mV/m, and the variational electric field was measured from 4 Hz to 1024 Hz.  The
dc electric field was measured at 16 samples/s.  The variational electric field
was measured from 1 microvolt/m to 10 mV/m rms. Additional details are found in
N. C. Maynard et al., Space Sci. Instrum., v. 5, n. 4, p. 523, 1981. The antenna
pair perpendicular to the orbit plane did not deploy.
 
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DE2_DCA500MS_VEFI doi:10.48322/0s61-a111
Description
The Vector Electric Field Instrument (VEFI) used flight-proven double-probe
techniques with 20-m baselines to obtain measurements of dc electric fields.
This electric field investigation had the following objectives: (1) to obtain
accurate and comprehensive triaxial dc electric field measurements at
ionospheric altitudes in order to refine the basic spatial patterns, define the
large-scale time history of these patterns, and study the small-scale temporal
and spatial variations within the overall patterns; (2) to study the degree to
which and in what region the electric field projects to the equatorial plane;
(3) to obtain measurements of extreme low frequency (ELF) and lower frequency
irregularity structures; and (4) to perform numerous correlative studies. The
instrument consisted of six cylindrical elements 11 m long and 28 mm in
diameter. Each antenna was insulated from the plasma except for the outer 2 m.
The baseline, or distance between the midpoints of these 2-m active elements,
was 20 m. The antennas were interlocked along the edges to prevent oscillation
and to increase their rigidity against drag forces. The basic electronic system
was very similar in concept to those used on IMP-J and ISEE 1, but modified for
a three-axis measurement on a nonspinning spacecraft. At the core of the system
were the high-impedance (1.E12 ohm) preamplifiers, whose outputs were accurately
subtracted and digitized (14-bit A/D conversion for sensitivity to about 0.1
microvolt/m) to maintain high resolution, for subsequent removal of the
cross-product of the vectors V and B in data processing. This provided the basic
dc measurement. Other circuitry was used to aid in interpreting the dc data and
to measure rapid variations in the signals detected by the antennas. The planned
dc electric field range was plus or minus 1 V/m, the planned resolution was 0.1
mV/m, and the variational electric field was measured from 4 Hz to 1024 Hz.  The
dc electric field was measured at 16 samples/s.  The variational electric field
was measured from 1 microvolt/m to 10 mV/m rms. Additional details are found in
N. C. Maynard et al., Space Sci. Instrum., v. 5, n. 4, p. 523, 1981. The antenna
pair perpendicular to the orbit plane did not deploy.
 
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DE2_DUCT16MS_RPA doi:10.48322/aab6-jj49
Description
The Retarding Potential Analyzer (RPA) measured the bulk ion velocity in the
direction of the spacecraft motion, the constituent ion concentrations, and the
ion temperature along the satellite path. These parameters were derived from a
least squares fit to the ion number flux vs energy curve obtained by sweeping or
stepping the voltage applied to the internal retarding grids of the RPA. In
addition, a separate wide aperture sensor, a duct sensor, was flown to measure
the spectral characteristics of iregularities in the total ion concentration.
The measured parameters obtained from this investigation were important to the
understanding of mechanisms that influence the plasma; i.e., to understand the
coupling between the solar wind and the earth's atmosphere. The measurements
were made with a multigridded planar retarding potential analyzer very similar
in concept and geometry to the instruments carried on the AE satellites. The
retarding potential was variable in the range from approximately +32 to 0 volts.
The details of this voltage trace, and whether it was continuous or stepped,
depended on the operating mode of the instrument. Specific parameters deduced
from these measurements were ion temperature; vehicle potential; ram component
of the ion drift velocity; the ion and electron concentration irregularity
spectrum; and the concentration of H+, He+, O+, and Fe+, and of molecular ions
near perigee. Additional details are in W. B. Hanson et al., Space Sci.
Instrum., v. 5, n. 4, p. 503, 1981.
It includes the DUCT portion of the high resolutiondata from the Dynamics
Explorer 2 (DE-2) Retarding Potential Analyzer (RPA) for the whole DE-2 mission
time period in ASCII format. This version was generated at NSSDC from the
PI-provided binary data (SPIO-00232). The DUCT files include RPA measurements of
the total ion concentration every 64 times per second. Due to a failure in the
instrument memory system RPA data are not available from 81317 06:26:40 UT to
82057 13:16:00 UT. This data set is based on the revised version of the RPA
files that was submitted by the PI team in June of 1995. The revised RPA data
include a correction to the spacecraft potential.
 
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DE2_ION2S_RPA doi:10.48322/41b3-kz41
Description
The Retarding Potential Analyzer (RPA) measured the bulk ion velocity in the
direction of the spacecraft motion, the constituent ion concentrations, and the
ion temperature along the satellite path. These parameters were derived from a
least squares fit to the ion number flux vs energy curve obtained by sweeping or
stepping the voltage applied to the internal retarding grids of the RPA. In
addition, a separate wide aperture sensor, a duct sensor, was flown to measure
the spectral characteristics of iregularities in the total ion concentration.
The measured parameters obtained from this investigation were important to the
understanding of mechanisms that influence the plasma; i.e., to understand the
coupling between the solar wind and the earth's atmosphere. The measurements
were made with a multigridded planar retarding potential analyzer very similar
in concept and geometry to the instruments carried on the AE satellites. The
retarding potential was variable in the range from approximately +32 to 0 volts.
The details of this voltage trace, and whether it was continuous or stepped,
depended on the operating mode of the instrument. Specific parameters deduced
from these measurements were ion temperature; vehicle potential; ram component
of the ion drift velocity; the ion and electron concentration irregularity
spectrum; and the concentration of H+, He+, O+, and Fe+, and of molecular ions
near perigee. Additional details are in W. B. Hanson et al., Space Sci.
Instrum., v. 5, n. 4, p. 503, 1981.
It includes the high-resolution data from the Dynamics Explorer 2 (DE-2)
Retarding Potential Analyzer (RPA) for the whole DE-2 mission time period in
ASCII format.  The ASCII version was generated at NSSDC from the PI-provided
binary data (SPIO-00232). The RPA data files include orbit parameters and
geophysical data at a time resolution of usually 2 seconds and sometimes 4
second. The following geophysical parameters are provided: ion drift vector, ion
density, ion temperature, spacecraft potential, ion densities of atomic oxygen,
hydrogen, helium, molecular constituents and high mass constituents, data
quality flag, and RMS error. The ion drift vector is given by its components in
spacecraft coordinates; the y and z components are IDM measurements. Due to a
failure in the instrument memory system RPA data are not available from 81317
06:26:40 UT to 82057 13:16:00 UT. This data set is based on the revised version
of the RPA files that was submitted by the PI team in June of 1995. The revised
RPA data include a correction to the spacecraft potential.
The Dynamics Explorer 2 Retarding Potential Analyzer (RPA) files contain the ion
temperature, the ion drift velocity along the sensor look direction, and the ion
composition and orbit parameters in ASCII format. The time resolution is
typically 2 seconds. Data are given as daily files (typically a few 100 Kbytes
each). NSSDC-developed software was used to read the RPA binary data and create
ASCII files.  For more on DE-2, RPA, and the binary data, see RPA_VOLDESC_DE.SFD
and RPA_FORMAT_DE.SFD. 
The RPA files are requested with the DATA_TYPE = RPA_ASCII and the ENTRY_ID =
yyddd and are then staged as yydddhhmm_RPA_DE_2S_V01.ASC; yy is the year, ddd is
the day of the year, hh is the hour, and mm is the minute of the starting time
of the data in the file.  The date range for the IDM files is 81218-83049 with
most days represented.
The data quality field contains a flag that describes the quality of the RPA
data.  A value greater than or equal to 0 indicates that the data has passed the
set of basic quality checks.  A negative value indicates that the RPA data fails
at least one check and is untrustworthy.  Following are the sequence of checks.
Tests are sequentially performed until a flag is assigned. 
   Ni<8000 or Ni>6.E6                 flag=-70
   Psi<-2 or Psi>0.5                  flag=-60
   for INVARIANT LATITUDE<50
      Ti<500 or Ti>10000              flag=-50
      |Vx|>700 m/s                    flag=-20
      Mols>O+                         flag=-40
       H+>O+                          flag=-30
       Vx=0                           flag= 40
       Vx non zero 
         Sum of light ions > 25% O+   flag= 50
         Sum of light ions < 25% O+   flag= 20
   set flag to 0 if one of the needed concentrations is unavailable.
   increase magnitude of flag by 5 if rms fit error > 10%
   for INVARIANT LATITUDE>50
      Ti<500 or Ti>200000             flag=-50
        Ti>7000
          |Vx|<1000 and |Vz|<1000     flag=-20
          Alt>600
            Mols>O+                   flag=-40
            O+>Mols                   flag= 30
          Alt<=600
           Mols>O+
             Vx>0                     flag=-10
             Vx<=0                    flag=  0
           O+>Mols                    flag= 30
        Ti<=7000
          |Vx|>2000                   flag=-20
          Mols>O+                     flag=-40
          O+>Mols                     flag= 60
   set flag to 0 if one of the needed concentrations is unavailable. Increase
magnitude of flag by 5 if rms fit error > 12%
The sweep type field contains a number (1 - 4) that represents the type of RPA
sweep used.  The sweep types are: 
  1. Integral RPA curve obtained with voltage sweep from 0 to beyond 10 volts.
  2. Electronic derivative of RPA curve obtained with voltage sweep from 0 to
beyond 10 volts.
  3. Integral RPA curve obtained with voltage sweep from 0 up to 8 volts.
  4. Electronic derivative of RPA curve obtained with voltage sweep from 0 to 8
volts.
 
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DE2_LAPI_ELECTRON-FLUX-COUNTS-PPS1
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
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DE2_LAPI_ELECTRON-FLUX-COUNTS-PPS2
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
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DE2_LAPI_GEIGER-MUELLER
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
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DE2_LAPI_GEIGER-MUELLER-RATIO
Description
The Low Altitude Plasma Instrument /LAPI/ The Low Altitude Plasma Instrument on
the Dynamics Explorer-B spacecraft provides high resolution velocity space
measurements of positive ions and electrons from 5 eV to 32 keV and a monitor of
electrons with energies above 35 keV. It consists of an array of 15 parabolic
electrostatic analyzers spanning 180 deg in angle and two Geiger-Mueller
counters mounted on a one-degree of freedom-scan platform. The platform is
controlled by a magnetometer that allows placement of the array to selected
angles with respect to the magnetic field. Each parabolic analyzer
simultaneously measures electrons and positive ions. The temporal resolution and
energy range of the measurements and the detector complement to be sampled are
programmable by ground command. 
1. The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
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DE2_LAPI_ION-FLUX-COUNTS-PPS1
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
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DE2_LAPI_ION-FLUX-COUNTS-PPS2
Description
The Low Altitude Plasma Instrument /LAPI/ The Low Altitude Plasma Instrument on
the Dynamics Explorer-B spacecraft provides high resolution velocity space
measurements of positive ions and electrons from 5 eV to 32 keV and a monitor of
electrons with energies above 35 keV. It consists of an array of 15 parabolic
electrostatic analyzers spanning 180 deg in angle and two Geiger-Mueller
counters mounted on a one-degree of freedom-scan platform. The platform is
controlled by a magnetometer that allows placement of the array to selected
angles with respect to the magnetic field. Each parabolic analyzer
simultaneously measures electrons and positive ions. The temporal resolution and
energy range of the measurements and the detector complement to be sampled are
programmable by ground command. 
1. The Instrument Data File Set. URL http://www.idfs.org 
Modification History
Initial Release
 
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DE2_LAPI_LAPI-MAG
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_ORBIT-ATTITUDE
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_ORBIT-ATTITUDE-MAGB
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_PITCH-ANGLES
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_PROJECTED-MAGB
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
Instruments abbreviations: 
FPI: Fabry-Perot Interferometer
IDM: Ion Drift Meter
LANG: Langmuir Probe
LAPI: Low Altitude Plasma Instrument
MAG-B: Magnetic Field Observations Triaxial Fluxgate Magnetometer
NACS: Neutral Atmosphere Composition Spectrometer
VEFI: Vector Electric Field Instrument
WATS: Wind and Temperature Spectrometer
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_SC-MAGB
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
Instruments abbreviations: 
FPI: Fabry-Perot Interferometer
IDM: Ion Drift Meter
LANG: Langmuir Probe
LAPI: Low Altitude Plasma Instrument
MAG-B: Magnetic Field Observations Triaxial Fluxgate Magnetometer
NACS: Neutral Atmosphere Composition Spectrometer
VEFI: Vector Electric Field Instrument
WATS: Wind and Temperature Spectrometer
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_LAPI_SHAFT-ENCODER-ANGLE
Description
The DE-2 spacecraft (low-altitude mission) complemented the high-altitude
mission DE-1and was placed into an orbit with a perigee sufficiently low to
permit measurements of neutral composition, temperature, and wind. The apogee
was high enough to permit measurements above the interaction regions of
suprathermal ions, and also plasma flow measurements at the feet of the
magnetospheric field lines. The general form of the spacecraft was a short
polygon 137 cm in diameter and 115 cm high. The triaxial antennas were 23 m
tip-to-tip. One 6-m boom was provided for remote measurements. The spacecraft
weight was 403 kg. Power was supplied by a solar cell array, which charged two
6-ampere-hour nickel-cadmium batteries. The spacecraft was three-axis stabilized
with the yaw axis aligned toward the center of the earth to within 1 deg. The
spin axis was normal to the orbit plane within 1 deg with a spin rate of one
revolution per orbit. A single-axis scan platform was included in order to mount
the low-altitude plasma instrument (81-070B-08). The platform rotated about the
spin axis. A pulse code modulation telemetry data system was used that operated
in real time or in a tape-recorder mode. Data were acquired on a
science-problem-oriented basis, with closely coordinated operations of the
various instruments, both satellites, and supportive experiments. Measurements
were temporarily stored on tape recorders before transmission at an 8:1
playback-to-record ratio. Since commands were also stored in a command memory
unit, spacecraft operations were not real time. Additional details can be found
in R. A. Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. DE-2
reentered the atmosphere on February 19, 1983. 
The Low-Altitude Plasma Instrument (LAPI) provided high-resolution velocity
space measurements of positive ions and electrons from 5 eV to 32 keV. The two
Geiger-Mueller counter tubes (0 and 90 deg) measured trapped electrons and
precipitating electrons above 35 keV as integral number flux. Pitch angle
measurements covered the full 180 deg range. Data from this investigation and
supporting measurements were used to study 
(1) the identification and intensities of Birkeland currents, 
(2) auroral particle source regions and acceleration mechanisms, 
(3) the existence and role of E parallel to B, 
(4) sources and effects of polar cap particle fluxes, 
(5) the transport of plasma within and through the magnetospheric cusp, 
(6) dynamic configurations of high-latitude flux tubes, 
(7) loss-cone effects of wave-particle interactions, 
(8) hot-cold plasma interactions, 
(9) ionospheric effects of particle precipitation, and 
(10) plasma convection at high altitudes. 
The instrument contained an array of 15 parabolic electrostatic analyzers of the
ISIS 2 type, each with an electron channel and an ion channel, in order to
obtain detailed pitch-angle distributions as a function of energy. Two
Geiger-Mueller counters were mounted on the scan platform. The basic mode of
operation provided a 32-point energy spectrum in the range 5 eV to 32 kev every
second. The voltages on the electrostatic analyzers were programmable to allow
for greater space/time resolution over limited portions of the energy and
angular distributions. The instrument was mounted on a one-axis scan platform
controlled by a magnetometer, whose purpose was to maintain the detector array,
which spanned 180 deg, at a nearly constant angle to the magnetic field.
Additional details are found in J. D. Winningham et al., Space Sci. Instrum., v.
5, n. 4, p. 465, 1981. From March 16, 1982 to April 4, 1982 the instrument was
turned off for corrective action. 
The Instrument Data File Set. URL http://www.idfs.org  
Modification History
Initial Release
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DE2_NEUTRAL1S_NACS doi:10.48322/j8kp-5y58
Description
The Neutral Atmosphere Composition Spectrometer (NACS) was designed to obtain in
situ measurements of the neutral atmospheric composition and to study the
variations of the neutral atmosphere in response to energy coupled into it from
the magnetosphere.  Because temperature enhancements, large-scale circulation
cells, and wave propagation are produced by energy input (each of which posseses
a specific signature in composition variation), the measurements permitted the
study of the partition, flow, and deposition of energy from the magnetosphere. 
Specifically, the investigation objective was to characterize the composition of
the neutral atmosphere with particular emphasis on variability in constituent
densities driven by interactions in the atmosphere, ionosphere, and
magnetosphere system. The quadrupole mass spectrometer used was nearly identical
to those flown on the AE-C, -D, and -E missions. The electron-impact ion source
was used in a closed mode. Atmospheric particles entered an antechamber through
a knife-edged orifice, where they were thermalized to the instrument
temperature. The ions with the selected charge-to-mass ratios had stable
trajectories through the hyperbolic electric field, exited the analyzer, and
entered the detection system. An off-axis beryllium-copper dynode multiplier
operating at a gain of 2.E6 provided an output pulse of electrons for each ion
arrival. The detector output had a pulse rate proportional to the neutral
density in the ion source of the selected mass. The instrument also included two
baffles that scanned across the input orifice for optional measurement of the
zonal and vertical components of the neutral wind. The mass select system
provided for 256 mass values between 0 and 51 atomic mass units (u) or each 0.2
u. It was possible to call any one of these mass numbers into each of eight
0.016-s intervals. This sequence was repeated each 0.128 s. More details are
found in G. R. Carignan et al., Space Sci. Instrum., v. 5, n. 4, p. 429, 1981.
This data set includes daily files of the PI-provided DE-2 NACS 1-second data
and corresponding orbit parameters.  The data set was generated at NSSDC from
the original PI-provided data and software (SPTH-00010) and from the
orbit/attitude database and software that is part of the DE-2 UA data set
(SPIO-00174). The original NACS data were provided by the PI team in a highly
compressed VAX/VMS binary format on magnetic tapes. The data set covers the
whole DE-2 mission time period. Each data point is an average over the normally
8 measurements per second. Densities and relative errors are provided for atomic
oxygen (O), molecular nitrogen (N2), helium (He), atomic nitrogen (N), and argon
(Ar).  The data quality is generally quite good below 500 km, but deteriorates
towards higher altitudes as oxygen and molecular nitrogen approach their
background values (which could only be determined from infrequent spinning
orbits) and the count rate for Ar becomes very low. The difference between
minimum (background) and maximum count rate for atomic nitrogen (estimated from
mass 30) was so small that results are generally poor.  Data were lost between
12 March 1982 and 31 March 1982 when the counter overflowed.
 
Dataset in CDAWeb
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DE2_NEUTRAL8S_FPI doi:10.48322/22v6-0p09
Description
The Fabry-Perot Interferometer (FPI) was a high-resolution remote sensing
instrument designed to measure the thermospheric temperature, meridional wind,
and density of the following metastable atoms: atomic oxygen (singlet S and D)
and the 2P state of ionic atomic oxygen. The FPI performed a wavelength analysis
on the light detected from the thermospheric emission features by spatially
scanning the interference fringe plane with a multichannel array detector. The
wavelength analysis characterized the Doppler line profile of the emitting
species. A sequential altitude scan performed by a commandable horizon scan
mirror provided a cross-sectional view of the thermodynamic and dynamic state of
the thermosphere below the DE 2 orbit. The information obtained from this
investigation was used to study the dynamic response of the thermosphere to the
energy sources caused by magnetospheric electric fields and the absorption of
solar ultraviolet light in the thermosphere. The instrument was based on the
visible airglow experiment (VAE) used in the AE program. The addition of a
scanning mirror, the Fabry-Perot etalon, an image plane detector, and a
calibration lamp were the principal differences. Interference filters isolated
lines at (in Angstroms) 5577, 6300, 7320, 5896, and 5200. The FPI had a field of
view of 0.53 deg (half-cone angle). More details are found in P. B. Hays et al.,
Space Sci. Instrum., v. 5, n. 4, p. 395, 1981. From February 16, 1982 to
September 11, 1982 the DE satellite was inverted and the FPI measured galactic
emissions.
NOTE: Animations of DE2-FPI science products have been created as daily summary
files. The animations contain binned averages displayed as a colour code against
a geographic background. The bin sizes are 7.5 deg latitude and 24.0 degree
longitude. The longitude bin corresponds to the approximate separation of
adjacent orbits, assuming that DE2 completed 15 orbits per day. The animations
are divided into day (06-18 LST) and night (18-06 LST). All summary file
information and animations employ spacecraft orbital attitude data. Users should
note 1) that the DE2-FPI experiment acquired airglow spectra by imaging the
terrestrial limb below and ahead of the spacecraft at an approximate tangent
altitude of 250 km; 2) all airglow spectra were acquired while the DE2
spacecraft orbited in it's normal configuration, which corresponded to calendar
months August to February in 1981/2 and 1982/3; 3) the orbital inclination of
DE2 was 90 degrees implying that DE2-FPI always viewed ahead along the meridian;
4) that DE2 flew in an elliptical orbit with perigee of 305 km and apogee of
1300 km at launch -- the altitude of DE2 for each FPI measurement is included
with each reduced data point permitting users to determine the tangent latitude
corresponding to the 250 km terrestrial airglow limb. The three gif animations
are: 
1. FPI_brightness.gif which documents the OI (6300A) column brightness in units
of log10 Rayleighs. Note different scales for day and night.
2. FPI_temperature.gif which documents the neutral thermosphere temperature in
units of degrees Kelvin.
3. FPI_wind.gif which documents the line of sight neutral wind component in
units of meters/second. The wind direction is positive when the wind blows away
from the approaching spacecraft.
 
Dataset in CDAWeb
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DE2_PLASMA500MS_LANG doi:10.48322/yq6h-5g10
Description
The Langmuir Probe Instrument (LANG) was a cylindrical electrostatic probe that
obtained measurements of electron temperature, Te, and electron or ion
concentration, Ne or Ni, respectively, and spacecraft potential.  Data from this
investigation were used to provide temperature and density measurements along
magnetic field lines related to thermal energy and particle flows within the
magnetosphere-ionosphere system, to provide thermal plasma conditions for
wave-particle interactions, and to measure large-scale and fine-structure
ionospheric effects of energy deposition in the ionosphere.  The Langmuir Probe
instrument was identical to that used on the AE satellites and the Pioneer Venus
Orbiter. Two independent sensors were connected to individual adaptive sweep
voltage circuits which continuously tracked the changing electron temperature
and spacecraft potential, while autoranging electrometers adjusted their gain in
response to the changing plasma density. The control signals used to achieve
this automatic tracking provided a continuous monitor of the ionospheric
parameters without telemetering each volt-ampere (V-I) curve.  Furthermore,
internal data storage circuits permitted high resolution, high data rate
sampling of selected V-I curves for transmission to ground to verify or correct
the inflight processed data. Time resolution was 0.5 seconds. More details are
in J. P. Krehbiel et al., Space Sci. Instrum., v. 5, n. 4, p. 493, 1981.
The Dynamics Explorer 2 Langmuir Probe (LANG) ASCII files contain the following
geophysical parameters: electron temperature, plasma density, and satellite
potential.  They also contain the most important DE-2 orbit parameters.  The
geophysical parameters in the ASCII files were derived.from the raw volt-ampere
data from LANG.  PI-provided software was used to convert the raw binary data
into the ASCII geophysical data.
 
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DE2_UA16S_ALL (spase://NASA/NumericalData/DE2/PT16S)
Description
This data set was generated at NSSDC from the DE-2 Unified Abstract (UA) data
and the DE-2 orbit/attitude data base and software. The daily UA files contain
16 second averages from the NACS, WATS, LANG, FPI and RPA/IDM instruments for
the whole DE-2 mission period.  The PI-provided data in VAX/VMS binary format
were converted to ASCII format and the most important orbit parameters were
added using the a/o data base and software provided by the DE project team.
Subsetting, plotting, and downloading (in ASCII format) capabilities for these
data are provided through the ATMOWeb interface at
https://nssdc.gsfc.nasa.gov/atmoweb/The ASCII are are also available from here:
https://spdf.gsfc.nasa.gov/pub/data/de/de2/ Each UA record contains the
following data: N2, O, He, Ar, and N densities [cm-3] from the Neutral
Atmosphere Composition Spectrometer (NACS), neutral temperature [K], eastward
and upward neutral wind [m/s] from the Wind and Temperature Spectrometer (WATS),
plasma density [cm-3] and electron temperature [K] from the Langmuir Probe
experiment (LANG), wavelength [A], tangent altitude [km], northward neutral wind
[m/s], neutral temperature [K], and intensity [Raleighs], from the Fabry
Interferometer (FPI), ion temperature [K], total ion density [cm-3], eastward,
northward, and upward ion drift [m/s] from the Retarding Potential Analyzer/Ion
Drift Meter (RPA/IDM). The IDM data entry is the revised version of June 1994.
Also included are the latitude, longitude, altitude, local time and other orbit
parameters. Higher time resolution data are available from NSSDC for the
individual experiments at https://spdf.gsfc.nasa.gov/pub/data/de/de2/ 
This investigation used data from several spacecraft instruments to study the
large-scale neutral-plasma interactions in the thermosphere caused by
magnetospheric-ionospheric and thermospheric coupling processes. Planned use of
the models is to provide a theoretical framework in which certain important
ionospheric and atmospheric properties needed for coupling processes (such as
the Pedersen and Hall conductivities) were consistently calculated using
satellite data measured at a given height. Planned examples are (1) to calculate
vertical profiles of ionospheric properties that were useful for comparison with
incoherent scatter radar measurements and other ground-based supporting data,
(2) to identify and evaluate the neutral thermospheric heat and momentum
sources, and (3) to determine the effectiveness of high-latitude dynamic
processes in controlling the global thermospheric circulation and thermal
structure.
 
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DE2_VION250MS_IDM doi:10.48322/reef-jt02
Description
The Ion Drift Meter (IDM) measured the bulk motions of the ionospheric plasma
perpendicular to the satellite velocity vector. The measured parameters,
horizontal and vertical ion-drift velocities, had an expected range of plus or
minus 4 km/s. The accuracy of the measurement was expected to be plus or minus
50 m/s for the anticipated 0.5 deg accuracy in vehicle attitude determination.
The nominal time resolution of the measurement was 1/32 s. This investigation
yielded information on (1) the ion convection (electric field) pattern in the
auroral and polar ionosphere; (2) the flow of plasma along magnetic field lines
within the plasmasphere, which determines whether this motion was simply a
breathing of the protonosphere, a refilling of this region after a storm, or an
interhemispheric transport of plasma; (3) the thermal ion contribution to
field-aligned electric currents; (4) velocity fields associated with small-scale
phenomena that are important at both low and high latitudes; and (5) the
magnitude and variation of the total concentration along the flight path. The
ion drift meter measured the plasma motion parallel to the sensor face by using
a gridded collimator and multiple collectors to determine the direction of
arrival of the plasma. The instrument geometry was very similar to that used on
the Atmosphere Explorer satellites. Each sensor consisted of a square entrance
aperture that served as collimator, some electrically isolating grids, and a
segmented planar collector. The angle of arrival of the ions with respect to the
sensor was determined by measuring the ratio of the currents to the different
collector segments, and this was done by taking the difference in the logarithms
of the current. Two techniques were used to determine this ratio. In the
standard drift sensor (SDS), the collector segments were connected in pairs to
two logarithmic amplifiers. The second technique, called the univeral drift
sensor (UDS), allowed simultaneous measurement of both components. Here, each
collector segment was permanently connected to a logarithmic amplifier and two
difference amplifiers were used to determine the horizontal and vertical arrival
angles simultaneously. The IDM consisted of two sensors, one providing the SDS
output and the other providing the UDS output. Further details are in R. A.
Heelis et al., Space Sci. Instrum., v. 5, n. 4, p. 511, 1981. During the period
from 81317 to 82057 the instrument memory suffered a critical upset and ion
temperatures and drifts are not available during this period.
This data set is available from here:
https://spdf.gsfc.nasa.gov/pub/data/de/de2/ It includes the high-resolution data
from the Dynamics Explorer 2 (DE-2) Ion Drift Meter (IDM) for the whole DE-2
mission time period in ASCII format. This data set was generated at NSSDC by
converting the PI-provided data set (SPIO-00232) from binary to ASCII format.
The IDM data files provide absolute measurements of the cross track ion drift
velocity 4 times per second. The complete drift vector can be obtained by
combining IDM and RPA ion drift measurements.
 
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DE2_WIND2S_WATS doi:10.48322/z50y-hd65
Description
The Wind and Temperature Spectrometer (WATS) measured the in situ neutral winds,
the neutral particle temperatures, and the concentrations of selected gases. The
objective of this investigation was to study the interrelationships among the
winds, temperatures, plasma drift, electric fields, and other properties of the
thermosphere that were measured by this and other instruments on the spacecraft.
Knowledge of how these properties are interrelated contributed to an
understanding of the consequences of the acceleration of neutral particles by
the ions in the ionosphere, the acceleration of ions by neutrals creating
electric fields, and the related energy transfer between the ionosphere and the
magnetosphere. Three components of the wind, one normal to the satellite
velocity vector in the horizontal plane, one vertical, and one in the satellite
direction were measured. A retarding potential quadrupole mass spectrometer,
coupled to the atmosphere through a precisely orificed antechamber, was used. It
was operated in either of two modes: one employed the retarding capability and
the other used the ion source as a conventional nonretarding source. Two
scanning baffles were used in front of the mass spectrometer: one moved
vertically and the other moved horizontally. The magnitudes of the horizontal
and vertical components of the wind normal to the spacecraft velocity vector
were computed from measurements of the angular relationship between the neutral
particle stream and the sensor. The component of the total stream velocity in
the satellite direction was measured directly by the spectrometer system through
determination of the required retarding potential.  At altitudes too high for
neutral species measurements, the planned operation required the instrument to
measure the thermal ion species only.  A series of four sequentially occurring
slots --each a 2-s long measurement interval-- was adapted for the basic
measurement format of the instrument. Different functions were commanded into
these slots in any combination, one per measurement interval. Thus the time
resolution can be 2, 4, 6, or 8 seconds.  Further details are found in N. W.
Spencer et al., Space Sci. Instrum., v. 5, n. 4, p. 417, 1981.
This data set consists of the high-resolution data of the Dynamics .Explorer 2
Wind and Temperature Spectrometer (WATS) experiment. The files contain the
neutral density, temperature and horizontal (zonal) wind velocity, and orbital
parameters in ASCII format. The time resolution is typically 2 seconds. Data are
given as daily files (typically a few 100 Kbytes each). PI-provided software
(WATSCOR) was used to correct the binary data set.  NSSDC-developed software was
used to add the orbit parameters, to convert the binary into ASCII format and to
combine the (PI-provided) orbital files into daily files. For more on DE-2,
WATS, and the binary data, see the WATS_VOLDESC_SFDU_DE.DOC and
WATS_FORMAT_SFDU_DE.DOC files. More information about the processing done at
NSSDC is given in WATS_NSSDC_PRO_DE.DOC.
 
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DE_UV_SAI doi:10.48322/t7ya-6231
Description
   Instrument functional description:
       The spin-scan auroral imagers (SAI) comprise three photometers which
   provide images of Earth at various wavelengths via interference filters
   mounted on a wheel and selected by ground command.  Two of the photometers
   provide visible wavelength images, and the third provides images at
   vacuum-ultraviolet wavelengths.
       The three photometers are mounted on the spacecraft such that their
   fields of view are separated by about 120 degrees in a plane oriented
   perpendicular to the spin axis.  Each photometer in operation collects
   one scan line during each spacecraft rotation, with an internal mirror
   stepping once per rotation to start a new scan line.
       An auroral image is a nadir-centered two-dimensional pixel array
   provided by the spacecraft rotation and the photometer's stepping mirror
   which advances the field of view 0.25 degrees once per rotation in a
   direction perpendicular to the plane of rotation.  A change in mirror-
   stepping direction signals the start of a new image.  One, two, or
   three photometers may be in operation at one time.  The images from all
   operating photometers are telemetered simultaneously with image repetition
   rates that typically vary from about 3 to 12 minutes.
       One of the three imaging photometers is equipped with filters and a
   photocathode for observations at vacuum-ultraviolet wavelengths, in
   particular emissions of the Lyman-Birge-Hopfield band of molecular
   nitrogen at about 140 to 170 nm.  Imaging at these wavelengths allows
   coverage of the auroral oval in both the dark and sunlit ionospheres.
   The filter array for the vacuum-ultraviolet imaging photometer also
   includes filters for atomic hydrogen Lyman alpha at 121.6 nm and oxygen
   lines at 130.4 and 135.6 nm.
       The full width of the fields of view of the photometers
   corresponding to a single pixel is 0.29 degrees.  An image frame
   consists of all scan lines obtained by mirror steps in one direction
   which deflect the field of view by 0.25 degrees per rotation.  The
   angular separation of two consecutive pixels in the direction of
   spacecraft rotation is about 0.23 degrees.  A full frame has 120
   scan lines or 30 degrees of width.  For routine processing the
   angular width along a scan line is 150 pixels, or about 34.5 degrees
   of length.  The frame width is occasionally adjusted to less than
   120 scan lines.
   Reference:
   Frank, L. A., J. D. Craven, K. L. Ackerson, M. R. English, R. H. Eather,
       and R. L. Carovillano, Global auroral imaging instrumentation for
       the Dynamics Explorer mission, Space Sci. Inst., 5, 369-393, 1981.
   Data set description:
       Each DE SAI UV image CDF contains all of images collected by the
   UV photometer during one day of operations.  The displayable image
   counts are in variable 3.
       Coordinates are calculated for each position of the image count array.
   These coordinates are in variables 14, 15, and 16.
       To facilitate viewing of the images, a mapping of pixel value to a
   recommended color table based on the characteristics of the selected
   filter will be included with each image.  See the description of variables
   17, 18, and 19 below.
       A relative intensity scale is provided by the uncompressed count
   table of variable 20.  Approximate intensity levels in kiloRayleighs are
   given in the intensity table of variable 21.
       Other variables provide orbit and attitude data and information about
   the selected filter and the mirror stepping direction.
 Variable descriptions:
  1,2. Start time
        The time assigned to an image is the start time of the initial scan
        line within a resolution of one second.
    3. Image counts
        Image pixel counts range from 0 to 255.  They are stored in a two-
        dimensional byte array of 121 columns by 150 rows.  Each column
        contains one scan line.  Images will generally not fill all of the
        121 columns.  When an image is displayed with row 1 at the top and
        column 1 on the left, the spacecraft spin axis is oriented to the
        left in the display, and the orbit normal vector is oriented to the
        right.
    4. Filter
        Twelve filters are available for ultra-violet imaging; the filter
        number, 1-12, is given here.  In addition, the peak wavelength in
        Angstroms is given for the selected filter.
    5. Presumed altitude of emissions
        The presumed altitude of the emissions seen in the image varies
        with the characteristics of the filter used.
  6,7. First and last mirror location counters (MLCs)
        The MLC range is from 28 in column 1 (leftmost) to 148 in column 121
        (rightmost).  The direction of mirror stepping motion is shown by
        comparing first and last MLCs.
    8. Orbit/attitude time
        Whenever possible, the approximate center time of the image is used
        for determining the orbit and attitude parameters.  If O/A data is
        not available for the center time, the closest available O/A time
        is used.
    9. Spacecraft position vector, GCI
   10. Spacecraft velocity vector, GCI
   11. Spacecraft spin axis unit vector, GCI
   12. Sun position unit vector, GCI
   13. Orbit normal unit vector, GCI
   14. Geographic longitude or right ascension
        East longitude is given for each image pixel on the Earth at the
        altitude given in variable 5.  When the pixel altitude is greater
        than the value of variable 5, the right ascension is given.
   15. Geographic latitude or declination
        North latitude is given for each image pixel on the Earth at the
        altitude given in variable 5.  When the pixel altitude is greater
        than the value of variable 5, the declination is given.
   16. Pixel altitude
        For each image pixel on the Earth, the presumed altitude of the
        emissions is used.  This is equal to the value of variable 5.  For each
        pixel off the Earth, the altitude of the line of sight is used.
   17. Pixel UT
        This array gives the start time for the collection of each image pixel.
   18. RGB color table
        This is the recommended color table to be used with the
        limits given in variables 19 and 20.
19,20. Low and high color mapping limits
        The low and high color limits are recommended for remapping
        the color table entries, as follows:
            For pixel values less than the low limit, use the color
                at table position 1.
            For pixel values greater than or equal to the low limit
                and less than or equal to the high limit, use the color
                at table position (pix-low)/(high-low) x 255 + 1.
            For pixel values greater than the high limit, use the color
                at table position 256.
   21. Expanded count table
        The image pixel counts are quasi-logarithmically compressed to the
        range 0-255.  This table gives the average of the uncompressed range
        for each compressed count value.  Table entries 1-128 correspond to
        compressed counts 0-127 respectively.  Count levels greater than
        127 are considered overflow.
   22. Intensity table
        For each of the twelve filters, approximate intensity levels in
        kiloRayleighs are given for each compressed count value.  Table
        entries 1-128 correspond to compressed counts 0-127 respectively.
        No count conversion data is available for count levels greater than
        127.
   Supporting software:
         Directions for obtaining supporting software is available on the SAI
   website at the URL .http://www-pi.physics.uiowa.edu/www/desai/software/. 
   Included is an IDL program that displays the images with the recommended
   color bar and provides approximate intensities and coordinate data for
   each pixel.
 
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DE_VS_EICS doi:10.48322/1gca-r323
Description
 Data: 96 second average fluxes for H+, O+, and He+ ions in 15 energy and 14
pitch angle bins. Including data uncertainties, data quality indicators and
spacecraft position information. 
References: 
1. Peterson, W.K., H.L. Collin, M.F. Doherty and C.M. Bjorklund, O+ and He+
restricted and extended (bi-modal) ion conic distributions, Geophys. Res.Lett.,
19, 1439, 1992. 
2. Collin, H.L., W.K. Peterson, J.F. Drake, and A.W. Yau, The helium components
of energetic terrestrial ion upflows: Their occurrence,  morphology, and
intensity, J. Geophys. Res., 93, 7558, 1988. 
3. Chiu, Y.T., R.M. Robinson, H.L. Collin, S. Chakrabarti, and G.R. Gladstone,
Exospheric imaging in the extreme ultraviolet, Geophys. Res. Lett., 17, 267,
1990. 
4. Robinson, R.M., Y.T. Chiu, R.C. Catura, H.L. Collin, D. Garrido and R. Smith,
Instrumental and observational requirements for space-based imaging of
magnetospheric emissions, Instrumentation for magnetospheric Imager, Proceedings
of the SPIE, The International Society for Optical Engineering,  Bellingham,
Washington, S. Chakrabarti, Ed., Vol. 1744, 13, 1992.
These data are are a validated sub set of the full resolution DE/EICS data set
archived in native VAX/VMS format at NSSDC under the DATA_SET_NAME: 
EICS_STAND_ALONE_TELEMETRY_FILE_SYSTEM. The data in this CDF are a super-set of
the data used to prepare the four large scale statistical studies referenced
above. 
The three data quality indicators N C and A described in the documentation
accompanying the EICS_STAND_ALONE_TELEMETRY_FILE_SYSTEM as well as several other
data quality and mode indicators are included here.  These data indicators are
described on line and are referenced from the DE project home page on the Space
Physics Data System.
URL: ftp://sierra.space..lockheed.com/DATA/de/DE_eics_home.html   IF Unavailable
try: http://leadbelley.lanl.gov/spds/project-pages-only.html 
Each physical cdf file contains data for an entire UT day.  The files have names
of the form YYDDD_EICS_DE.cdf
The file naming convention includes the UT day encoded in the NASA standard
YYDDD format. YY are the last two digits of the year and DDD is the day of year
with January 1 = 001. 
EICS data were not acquired in all 24 UT day intervals. If no input data were
available for a UT day period, no CDF file was produced.  IFEICS data were
available but there are no data available stisfying the input requirements for
this data set for a UT day interval, the CDF file contains one record of
CDF_FILL data entries for all record variable entries. 
Metadata providedby W.K. Peterson with the helpof Mona Kessel
Modification History
Created October, 1995 by W.K. Peterson
Add Q_FLAG_FILE_CORRUPTED variable to indicate intervals for which full data
quality information is not available. 10/10/95 
 
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DMSP-F06_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F07_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F08_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F09_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F12_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F13_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
Version 1.1.2
Added ORBIT_INDEX and AURORAL_REGION variables
Version 1.1.3
Added AURORAL_BOUNDARY_FOM figure of merit for dynamic auroral boundary
determination variable
Version 1.1.4
Removed AURORAL_REGION and AURORAL_BOUNDARY_FOM variables. See
github.com/lkilcommons/ssj_auroral_boundary
Version 1.1.5
Removed ORBIT_INDEX to make compatible with CDAWeb 1,1,2 master CDF
 
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DMSP-F14_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F15_SSJ_PRECIPITATING-ELECTRONS-IONS
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F16_SSIES-3_THERMAL-PLASMA doi:10.48322/hcdm-vz96
Proper citations should include the "Accessed on date" in the form .
Description
The Special Sensors-Ions, Electrons, and Scintillation (SSIES) thermal plasma
analysis package is a suite of instruments built by the Center for Space
Sciences at the University of Texas at Dallas and flown on a number of the DMSP
satellites. SSIESS includes a Retarding Potential Analyzer (RPA), Ion Drift
meter (IDM), scintillation meter, and Langmuir probe.
 
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DMSP-F16_SSJ_PRECIPITATING-ELECTRONS-IONS doi:10.48322/1rnz-f067
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F16_SSM_MAGNETOMETER doi:10.48322/bh8f-yy31
Description
Magetic measurements taken at nominally 850km altitude using a 3-axis fluxgate
magnetometer.  Please contact Rob.Redmon@noaa.gov or
liam.kilcommons@colorado.edu with questions and comments. Many individuals made
important contributions including: F. Rich, G. Wilson, D. Ober, R. Redmon, D.
Knipp, L. Kilcommons, P. Alken.
Modification History
This is version 1, beta.
Version 1.0.1
Apex and geocentric east-north-up coordinates added. Polynomial baseline
corrected versions of perturabtions added.
Version 1.0.2
Auroral region (from SSJ boundary identification) and orbit index added 
Version 1.0.3
Added Spacecraft Along Track Unit Vector
Switched naming convention from corrected ending in _COR to original ending in
_ORIG, so that MFIT corrected data would appear to be default. Removed any
variables that were uncorrected except for spacecraft coordinates.
Version 1.0.4
Added recomputed magnetic perturbations, i.e. recomputed the IGRF field for the
improved locations, and subtracted it from the observed total field. Added
spacecraft across track unit vector. Switch SC_APEX_LON to -180. to 180. instead
of 0.-360.
 
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DMSP-F17_SSIES-3_THERMAL-PLASMA doi:10.48322/3skz-xt83
Proper citations should include the "Accessed on date" in the form .
Description
The Special Sensors-Ions, Electrons, and Scintillation (SSIES) thermal plasma
analysis package is a suite of instruments built by the Center for Space
Sciences at the University of Texas at Dallas and flown on a number of the DMSP
satellites. SSIESS includes a Retarding Potential Analyzer (RPA), Ion Drift
meter (IDM), scintillation meter, and Langmuir probe.
 
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DMSP-F17_SSJ_PRECIPITATING-ELECTRONS-IONS doi:10.48322/zjs1-0y88
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F17_SSM_MAGNETOMETER doi:10.48322/1c9w-jd85
Description
Magetic measurements taken at nominally 850km altitude using a 3-axis fluxgate
magnetometer.  Please contact Rob.Redmon@noaa.gov or
liam.kilcommons@colorado.edu with questions and comments. Many individuals made
important contributions including: F. Rich, G. Wilson, D. Ober, R. Redmon, D.
Knipp, L. Kilcommons, P. Alken.
Modification History
This is version 1, beta.
Version 1.0.1
Apex and geocentric east-north-up coordinates added. Polynomial baseline
corrected versions of perturabtions added.
Version 1.0.2
Auroral region (from SSJ boundary identification) and orbit index added 
Version 1.0.3
Added Spacecraft Along Track Unit Vector
Switched naming convention from corrected ending in _COR to original ending in
_ORIG, so that MFIT corrected data would appear to be default. Removed any
variables that were uncorrected except for spacecraft coordinates.
Version 1.0.4
Added recomputed magnetic perturbations, i.e. recomputed the IGRF field for the
improved locations, and subtracted it from the observed total field. Added
spacecraft across track unit vector. Switch SC_APEX_LON to -180. to 180. instead
of 0.-360.
 
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DMSP-F18_SSIES-3_THERMAL-PLASMA doi:10.48322/cxc3-w323
Proper citations should include the "Accessed on date" in the form .
Description
The Special Sensors-Ions, Electrons, and Scintillation (SSIES) thermal plasma
analysis package is a suite of instruments built by the Center for Space
Sciences at the University of Texas at Dallas and flown on a number of the DMSP
satellites. SSIESS includes a Retarding Potential Analyzer (RPA), Ion Drift
meter (IDM), scintillation meter, and Langmuir probe.
 
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DMSP-F18_SSJ_PRECIPITATING-ELECTRONS-IONS doi:10.48322/34mn-w272
Description
Precipitating electrons and ions observed at nominally 850km altitude and over a
range of energies from 30 eV to 30 keV using the Special Sensor J (SSJ)
instrument.  Please contact Rob.Redmon@noaa.gov with questions and comments.
Many individuals made important contributions including: D. Hardy, E. Holeman,
F. Rich, D. Ober, G. Wilson, J. Machuzak, K. Kadinsky-Cade, J. McGarity, W.F.
Denig, K. Martin, R. Redmon, D. Knipp, L. Kilcommons.
Modification History
This is version 1, beta.
 
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DMSP-F18_SSM_MAGNETOMETER doi:10.48322/cj1v-6g43
Description
Magetic measurements taken at nominally 850km altitude using a 3-axis fluxgate
magnetometer.  Please contact Rob.Redmon@noaa.gov or
liam.kilcommons@colorado.edu with questions and comments. Many individuals made
important contributions including: F. Rich, G. Wilson, D. Ober, R. Redmon, D.
Knipp, L. Kilcommons, P. Alken.
Modification History
This is version 1, beta.
Version 1.0.1
Apex and geocentric east-north-up coordinates added. Polynomial baseline
corrected versions of perturabtions added.
Version 1.0.2
Auroral region (from SSJ boundary identification) and orbit index added 
Version 1.0.3
Added Spacecraft Along Track Unit Vector
Switched naming convention from corrected ending in _COR to original ending in
_ORIG, so that MFIT corrected data would appear to be default. Removed any
variables that were uncorrected except for spacecraft coordinates.
Version 1.0.4
Added recomputed magnetic perturbations, i.e. recomputed the IGRF field for the
improved locations, and subtracted it from the observed total field. Added
spacecraft across track unit vector. Switch SC_APEX_LON to -180. to 180. instead
of 0.-360.
 
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DMSPF16_R0_SSUSI
Description
No TEXT global attribute value.
 
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DMSPF17_R0_SSUSI
Description
No TEXT global attribute value.
 
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DMSPF18_R0_SSUSI
Description
No TEXT global attribute value.
 
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DMSP_R0_SSIES
Description
No TEXT global attribute value.
 
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DMSP_R0_SSJ4
Description
No TEXT global attribute value.
 
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DN_K0_GBAY (spase://GBO/NumericalData/DARN/GooseBay/PT2M)
Description
vlptm $Revision: 4.3
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_HANK (spase://GBO/NumericalData/DARN/Hankasalmi/PT2M)
Description
vlptm $Revision: 4.5
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_ICEW (spase://GBO/NumericalData/DARN/Stokkseyri/PT2M)
Description
vlptm $Revision: 4.3
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_KAPU (spase://GBO/NumericalData/DARN/Kapuskasing/PT2M)
Description
vlptm $Revision: 4.3
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_PACE (spase://GBO/NumericalData/DARN/HalleyBay/PT2M)
Description
vlptm version 2.42
Ref1: Satellite Experiments Simultaneous with Antarctic Measurements (SESAME) 
to be submitted to Reviews of Geophysics (copy held by GGS group at NASA)
Ref2:Baker et al.,EOS 70,p785 1989. Ref3: Greenwald et al.,Radio Sci.20,p63 1985
Info:Keith Morrison,GGS Scientist,British AntarcticSurvey,Cambridge,CB3 0ET,UK
E-mail: 19989::MORRISON
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_PYKK (spase://GBO/NumericalData/DARN/Pykkvibaer/PT2M)
Description
vlptm $Revision: 4.5
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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DN_K0_SASK (spase://GBO/NumericalData/DARN/Saskatoon/PT2M)
Description
vlptm $Revision: 4.3
Modification History
skeleton table implemented 
new formats with all the DEPEND attrs set
ISTP KPGS Standard & Conventions version 1 implemented
 
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Data Access Code Examples written in Python and IDL®.
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DN_MAGN-L2-HIRES_G08
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
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DN_MAGN-L2-HIRES_G09
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
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DN_MAGN-L2-HIRES_G10
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DN_MAGN-L2-HIRES_G11
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DN_MAGN-L2-HIRES_G12
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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DN_MAGN-L2-HIRES_G13
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
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DN_MAGN-L2-HIRES_G14
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
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DN_MAGN-L2-HIRES_G15
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
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DN_MAGN-L2-HIRES_G16
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
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DN_MAGN-L2-HIRES_G17
Description
Magnetometer high-resolution data for the GOES-8 through GOES-17, (GOES I-M,
GOES-NOP and GOES-R series of 10 spacecraft). The GOES MAG subsystem consists of
fluxgate magnetometer instruments monitoring three orthogonal components of the
geomagnetic field at geosynchronous orbit (L = 6.6) with high resolution
sampling rate (G8-15: 2 Hz and G16-17: 10 Hz). The NetCDF product files include
the magnetometer observations from the instrument(s) in several coordinate
systems, and the satellite location calculated using a standard SGP/SDP orbit
propagator. The field measurements are provided as B field vectors in the ECI
(Earth-centered inertial), EPN (earthward, poleward, normal/eastward), GSE
(geocentric solar ecliptic), GSM(geocentric solar magnetospheric) and VDH
(dipole aligned) coordinate systems. For comprehensive documentation including
caveats and usage recommendations, please consult the GOES magnetometer User's
Guide at NCEI. 
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
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DN_MAGN-L2-HIRES_G18
Description
The GOES-R spacecraft includes a pair of boom-mounted fluxgate magnetometer
instruments which operate simultaneously to obtain measurements of the
geomagnetic field. The Magnetometer Subsystem supports the following mission
objectives: 1) Map the space environment that controls charged particle dynamics
in the outer region of the magnetosphere, 2) Measure the magnitude and direction
of the Earth's ambient magnetic field in three orthogonal directions in the
geosynchronous equatorial orbit, 3) Determine general level of geomagnetic
activity, and 4) Detect magnetopause crossings, storm sudden commencements, and
substorms. The product described in this file includes the magnetometer
observations in several coordinate systems.
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
Dataset in CDAWeb
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DN_MAGN-L2-HIRES_G19
Description
The GOES-R spacecraft includes a pair of boom-mounted fluxgate magnetometer
instruments which operate simultaneously to obtain measurements of the
geomagnetic field. The Magnetometer Subsystem supports the following mission
objectives: 1) Map the space environment that controls charged particle dynamics
in the outer region of the magnetosphere, 2) Measure the magnitude and direction
of the Earth's ambient magnetic field in three orthogonal directions in the
geosynchronous equatorial orbit, 3) Determine general level of geomagnetic
activity, and 4) Detect magnetopause crossings, storm sudden commencements, and
substorms. The product described in this file includes the magnetometer
observations in several coordinate systems.
Modification History
SPDF added to master VAR_TYPE, Mission_group, Instrument_type and use of mapping
file to map attributes to ISTP equivalents
Also need to add Logical_source, Logical_source_description, Source_name and
virtual variable Epoch and time_base variable.
Also need to add FORMAT, VAR_NOTES, LABLAXIS, LABL_PTR_1, DISPLAY_TYPE variable
attributes and values
Also added validmin and max values for the b_quality variable
 
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DSCOVR_AT_DEF (spase://NOAA/NumericalData/DSCOVR/Ephemeris/Attitude/Definitive/PT5S)
Description
DSCOVR 3-axis stabilized definitive Attitude data file.
5 second time resolution
Convention: intrinsic rotations applied in Yaw, Pitch, Roll order
Extended Kalman Filter applied to ground based solution during normal
operations. OBC solution used during calibration maneuvers.
Modification History
08/02/2017 Initial Release
 
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DSCOVR_AT_PRE (spase://NOAA/NumericalData/DSCOVR/Ephemeris/Attitude/Preliminary/PT10S)
Description
DSCOVR 3-axis stabilized preliminary Attitude data file.
Time resolution varies.
Convention: intrinsic rotations applied in Yaw, Pitch, Roll order
 5 point Median Filter applied to DCM matrix
Modification History
8/29/2016 - Original Implementation
 
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DSCOVR_H0_MAG (spase://NOAA/NumericalData/DSCOVR/PlasMag/FluxgateMagnetometer/CDF/PT1S)
Description
DSCOVR Fluxgate Magnetometer 1-sec Definitive Data                              
Modification History
12/01/2016 Initial release
 
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DSCOVR_H1_FC (spase://NOAA/NumericalData/DSCOVR/PlasMag/FaradayCup/CDF/PT1M)
Description
Best fit parameters from nonlinear fitting of a single, isotropic Maxwellian
velocity distribution function to sets of DSCOVR Faraday Cup measurements of the
solar wind thermal proton peak. 1-minute resolution data are obtained by fitting
to the 1-minute integrated distributions, comprising ~15 as-measured charged
current spectra each. Reported uncertainties are fitting uncertainties, which do
not account for so-called prior uncertainties associated with non-Maxwellian
distributions in nature or with conditions that vary on timescales faster than 1
minute. The uncertainties associated with measurement of charged flux as a
function of energy are propagated. Certain empirical corrections have been
applied.
Modification History
V01: 10-MAR-2017
V02: 24-MAR-2017
V03: 30-MAY-2017
V04: 14-JULY-2017
V05: 30-JULY-2017
V06: 23-OCT-2017
 
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DSCOVR_ORBIT_PRE (spase://NOAA/NumericalData/DSCOVR/Ephemeris/Orbit/Preliminary/PT1M)
Description
DSCOVR Predicted Orbit data file.
 
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DYNAMO-2_DESA_NX02A-ESA-FLUX
Description
The DYNAMO-2 Dual Electrostatic Analyzer (DESA) instrument consisted of a single
boom-mounted prototype sensor (DESA-NX-02A), and a main electronics box (MEB).
The instrument was flown primarily as an engineering test flight of the DESA
sensor and was only flown aboard the second of the two DYNAMO-2 rockets
(35.357). The instrument had a single fixed field-of-view looking up towards
space along the spin-axis of the rocket. For full details of the instrument, see
Collinson et al., (2022). The instrument was configured as a low-energy
photoelectron spectrometer.
 
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EARTH_HELIO1DAY_POSITION (spase://NASA/NumericalData/Planet/Earth/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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EARTH_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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ELA_L1_EPDEF doi:10.48322/jyaq-cq12
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2018-07-20
 
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ELA_L1_EPDIF doi:10.48322/csjm-bk25
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2018-07-20
 
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ELA_L1_STATE_DEFN
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2022-09-25
 
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ELA_L1_STATE_PRED
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2022-09-17
 
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ELB_L1_EPDEF doi:10.48322/w4ac-2h02
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2018-07-20
 
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ELB_L1_EPDIF doi:10.48322/0etj-j292
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2018-07-20
 
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ELB_L1_STATE_DEFN
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2022-09-28
 
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ELB_L1_STATE_PRED
Description
The Electron Losses and Fields Investigation (ELFIN) mission is a space weather
mission using three scientific instruments in a 3U+ CubeSat. The instruments
measure wave and particle data.
Modification History
Rev- 2022-09-27
 
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ENDURANCE_EPHEMERIS_DEF
Description
No TEXT global attribute value.
 
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ENDURANCE_EPHEMERIS_GPS
Description
Data from the GPS receiver aboard Endurance plus a conversion of the coordinates
into magnetic latitude and longitude
 
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ENDURANCE_FIELDS_SKINPOT-500US
Description
TM1 electric field sphere potential (skins) voltages from Endurance FIELDS
experiment during flight.
 
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ENDURANCE_FIELDS_VLF-33US
Description
TM1 electric field sphere differential voltages from Endurance FIELDS experiment
during flight.
 
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ENDURANCE_L1A_PES
Description
No TEXT global attribute value.
 
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ENDURANCE_L1B_PES
Description
The Endurance PES instrument was comprised of 8 boom-mounted Dual Electrostatic
Analyzer (DESA) sensors, and a main electronics box (MEB). Each DESA sensor had
two look directions; A-side (looking down to Earth from launch to pitch-over
maneuver, and then up to space until loss of signal (LOS)); and B-side (looking
up to space from launch to pitch-over, and then down to Earth until loss of
signal (LOS)). The sensors were synchronized by the MEB and cross-calibrated to
look at approximately the same energy at the same time. A PES sweep consisted of
81 different steps and took 10 seconds. At each step, a voltage could be applied
to the Electrostatic Analyzer (ESA) and/or the Retarding Potential Analyzer
(RPA). Of these 81 steps; 3 (0, 1, 44) were used to take background counts with
the ESA grounded, and to fire the SLP; 34 (2:9, 33, 56:80) were used to collect
the standard resolution data measurement (15% DE/E, 10eV to 1keV) using the ESA
alone; and 44 (10:32, 34:43, 45:55) were used to collect the high-resolution
measurement (0.5% DE/E, 20.3 eV to 25.85 eV) using the ESA and RPA combined.”
 
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ENDURANCE_L2-ESA_PES
Description
The Endurance PES instrument was comprised of 8 boom-mounted Dual Electrostatic
Analyzer (DESA) sensors, and a main electronics box (MEB). Each DESA sensor had
two look directions; A-side (looking down to Earth from launch to pitch-over
maneuver, and then up to space until loss of signal (LOS)); and B-side (looking
up to space from launch to pitch-over, and then down to Earth until loss of
signal (LOS)). The sensors were synchronized by the MEB and cross-calibrated to
look at approximately the same energy at the same time. These data present the
standard resolution data measurement (15% DE/E, 10eV to 1keV) using the ESA
alone, using counts from all the sensors combined together.
 
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ENDURANCE_L2-GF_PES
Description
The Endurance PES instrument was comprised of 8 boom-mounted Dual Electrostatic
Analyzer (DESA) sensors, and a main electronics box (MEB). Each DESA sensor had
two look directions; A-side (looking down to Earth from launch to pitch-over
maneuver, and then up to space until loss of signal (LOS)); and B-side (looking
up to space from launch to pitch-over, and then down to Earth until loss of
signal (LOS)). The sensors were synchronized by the MEB and cross-calibrated to
look at approximately the same energy at the same time. A PES sweep consisted of
81 different steps and took 10 seconds. At each step, a voltage could be applied
to the Electrostatic Analyzer (ESA) and/or the Retarding Potential Analyzer
(RPA). Of these 81 steps; 3 (0, 1, 44) were used to take background counts with
the ESA grounded, and to fire the SLP; 34 (2:9, 33, 56:80) were used to collect
the standard resolution data measurement (15% DE/E, 10eV to 1keV) using the ESA
alone; and 44 (10:32, 34:43, 45:55) were used to collect the high-resolution
measurement (0.5% DE/E, 20.3 eV to 25.85 eV) using the ESA and RPA combined.
These calibration data present the variation in Geometric Factor with PES
operation during flight
 
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ENDURANCE_L2-RPA_PES
Description
The Endurance PES instrument was comprised of 8 boom-mounted Dual Electrostatic
Analyzer (DESA) sensors, and a main electronics box (MEB). Each DESA sensor had
two look directions; A-side (looking down to Earth from launch to pitch-over
maneuver, and then up to space until loss of signal (LOS)); and B-side (looking
up to space from launch to pitch-over, and then down to Earth until loss of
signal (LOS)). The sensors were synchronized by the MEB and cross-calibrated to
look at approximately the same energy at the same time. These data present the
high-resolution measurement (0.5% DE/E, 20.3 eV to 25.85 eV) using the ESA and
RPA counts from all the sensors combined together
 
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ENDURANCE_L2_SLP
Description
The Endurance SLP was a needle probe mounted on the forward Fo’c’sle of the
spacecraft. It measured thermal plasma density, electron temperature, the
potential difference between the spacecraft and ambient plasma (plasma
potential) and the relative potential of the spacecraft. SLP performed an active
(20ms) sweep once every 5 seconds, wherein a sweeping +/- 5V voltage was applied
to the needle. The data products here were derived from the I-V curves and
intercalibrated with EISCAT Radar and the PES instrument.
 
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ENDURANCE_L2_SLP_PSD
Description
The Sweeping Langmuir Probe is a traditional Langmuir probe with a sweep voltage
of +/-5V is applied to a gold plated cylinder.  Besides generating I-V curves to
derive electron temperature, ion and electron density and spacecraft floating
potential, spectra were obtained with a duty cycle of once per 5 seconds.
 
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ENDURANCE_L3_PES
Description
The Endurance mission was designed to make the first measurement of Earth’s
electric potential. This Level 3 data product is the potential drop below
Endurance as measured from the shift in the peak of the N2 A2 Πu  He-II
photopeak, corrected for spacecraft potential by the Swept Langmuir Probe. 
 
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EQ_PP_AUX (spase://ESA/NumericalData/Equator-S/Ephemeris/PrimeParameter/PT4S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.8 AUX
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
 No caveats
 
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EQ_PP_EDI (spase://ESA/NumericalData/Equator-S/EDI/PP/PT60s)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.2 EDI
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Caveats
 No caveats
 
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EQ_PP_EPI (spase://ESA/NumericalData/Equator-S/EPI/PP/PT60S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.5 EPI
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
* 1997 Dec - first release v1.0
* 1998 Apr - v1.4 PPDB Production Release
* 1998 Dec - v2.0
Caveats
See also `TEXT' global attr. for Caveats file location
 
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EQ_PP_ICI (spase://ESA/NumericalData/Equator-S/ICI/PP/PT60S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.3 ICI
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
none
Caveats
 This file has particularly bad background problems due to intense
 radiation belts from ~08:00-10:00 UT.
 This file contains both onboard calculated moments (labeled 
 "raw" with an "*" in the name) and moments calculated on 
 the ground from 3D distributions (labeled "final").
 Quantitative analysis should be done with the "final" moments.  
 The raw data should only be used qualitatively for identifying
 regions and temporal variations.  It has large errors, particularly
 in Vz in spacecraft coordinates.
 O+ and He+ data should not be used in the magnetosheath or at low
 L-values, due to background problems.
 Contact the LI at Lynn.Kistler@unh.edu if the data you need
 is not available on-line.
 
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EQ_PP_MAM (spase://ESA/NumericalData/Equator-S/MAM/PP/PT60S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.1 MAM
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
MAM_SINGLE (128 Hz) and MAM_DUAL (64 Hz) instrument acquisition modes are
available
Caveats
 no valid data 
 
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EQ_PP_PCD (spase://ESA/NumericalData/Equator-S/PCD/PP/PT60S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.6 PCD
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
Record of history of modification of CDF n/a.
Caveats
 partly noisy data
 noisy data
 
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EQ_SP_SFD (spase://ESA/NumericalData/Equator-S/SFD/PP/PT60S)
Description
see EQS-MPE-EDC-01, Equator-S Data Center Manual, section 4.7 SFD
Modification History
Produced in accordance with ESDS file specification
Reference Document for CSDS CDF File Design, DS-QMW-TN-0003
none
Caveats
 The used electron sensitivity 4.3e-7 A/(W/cm2) results from
 questionable calibration.  The resulting upper limits for
 electron energy fluxes are too high.
 
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ERG_HEP_L2_OMNIFLUX
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_LEPE_L2_OMNIFLUX
Description
No TEXT global attribute value.
Modification History
Created 10/2023
 
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ERG_LEPI_L2_OMNIFLUX
Description
filled in with information  
Modification History
Created 06/2024
 
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ERG_MEPE_L2_3DFLUX
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_MEPE_L2_OMNIFLUX
Description
" "
Modification History
Created 12/2024
 
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ERG_MEPI_L2_3DFLUX
Description
" "
Modification History
Created 10/2025
 
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ERG_MEPI_L2_OMNIFLUX
Description
" "
Modification History
Created 10/2025
 
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ERG_MGF_L2_8SEC doi:10.34515/data.erg-06001
Proper citations should include the "Accessed on date" in the form .
Description
For the calculation of the IGRF field, IDL Geopack v10.9 and IGRF-13 were used.
Modification History
Created 12/2024
 
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ERG_ORB_L2
Description
ERG orbit
Modification History
Created 12/2025
 
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ERG_ORB_LPRE_L2
Description
Predicted ERG orbit
Modification History
Created 10/2024
 
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ERG_ORB_MPRE_L2
Description
Predicted ERG orbit
Modification History
Created 12/2025
 
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ERG_ORB_PRE_L2
Description
Predicted ERG orbit
Modification History
Created 12/2025
 
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ERG_ORB_SPRE_L2
Description
Predicted ERG orbit
Modification History
Created 12/2025
 
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ERG_PWE_EFD_L2_E_SPIN
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_PWE_EFD_L2_POT
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_PWE_HFA_L2_SPEC_HIGH
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_PWE_HFA_L2_SPEC_LOW
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_PWE_HFA_L2_SPEC_MONIT
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_PWE_OFA_L2_SPEC doi:10.34515/data.erg-08000
Proper citations should include the "Accessed on date" in the form .
Description
No TEXT global attribute value.
Modification History
Created 12/2024
 
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ERG_XEP_L2_OMNIFLUX
Description
No TEXT global attribute value.
Modification History
Created 06/2024
 
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FAST_HR_DCB doi:10.48322/86pq-hb06
Description
Calibrated fluxgate magnetometer data acquired by the Fast Auroral SnapshoT
Small Explorer (FAST). Data have been calibrated, despun, and detrended against
the International Geomagnetic Reference Field (IGRF), using IGRF coefficients
for the date of acquisition. Data are provided in several coordinate systems.
Non detrended data in spacecraft and Geocentric Equatorial Inertial coordinates
are also provided. Ephemeris data are provided.
Modification History
Initial CDF development 8/14/12
Version 1 release 03/07/13
Updated to CDF version 3.5.0 11/26/13
Version 2 release 08/18/14
Updated to CDF Version 3.6.0 6/16/15
Updated to CDF Version 3.8.0.1 8/23/20
 
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FAST_OR_SSC
Description
GROUP 1    Satellite   Resolution   Factor
            fast           60         1
           Start Time           Stop Time 
           1996 235 00:00       2009 124 00:00   
Coord/            Min/Max   Range Filter       Filter
Component   Output Markers  Minimum  Maximum   Mins/Maxes 
GEO X        YES      -         -           -             -         -           
 -   
GEO Y        YES      -         -           -             -         -           
 -   
GEO Z        YES      -         -           -             -         -           
 -   
GEO Lat      YES      -         -           -             -         -           
 -   
GEO Lon      YES      -         -           -             -         -           
 -   
GEO LT       YES      -         -           -             -         -           
 -   
GM X         YES      -         -           -             -         -           
 -   
GM Y         YES      -         -           -             -         -           
 -   
GM Z         YES      -         -           -             -         -           
 -   
GM Lat       YES      -         -           -             -         -           
 -   
GM Lon       YES      -         -           -             -         -           
 -   
GM LT        YES      -         -           -             -         -           
 -   
GSE X        YES      -         -           -             -         -           
 -   
GSE Y        YES      -         -           -             -         -           
 -   
GSE Z        YES      -         -           -             -         -           
 -   
GSE Lat      YES      -         -           -             -         -           
 -   
GSE Lon      YES      -         -           -             -         -           
 -   
GSE LT       YES      -         -           -             -         -           
 -   
GSM X        YES      -         -           -             -         -           
 -   
GSM Y        YES      -         -           -             -         -           
 -   
GSM Z        YES      -         -           -             -         -           
 -   
GSM Lat      YES      -         -           -             -         -           
 -   
GSM Lon      YES      -         -           -             -         -           
 -   
SM X         YES      -         -           -             -         -           
 -   
SM Y         YES      -         -           -             -         -           
 -   
SM Z         YES      -         -           -             -         -           
 -   
SM Lat       YES      -         -           -             -         -           
 -   
SM Lon       YES      -         -           -             -         -           
 -   
SM LT        YES      -         -           -             -         -           
 -   
Addtnl             Min/Max      Range Filter          Filter
Options     Output Markers    Minimum     Maximum    Mins/Maxes
dEarth       YES      -         -           -             -   
MagStrgth    YES      -         -           -             -   
dNeutS       YES      -         -           -             -   
dBowSck      YES      -         -           -             -   
dMagPause    YES      -         -           -             -   
L_Value      YES      -         -           -             -   
InvarLat     YES      -         -           -             -   
Perform the following magnetic field traces:   
    North trace for GEO footpoint; Output: lat, lon, arclen.
    South trace for GEO footpoint; Output: lat, lon, arclen.
    North trace for GM footpoint; Output: lat, lon, arclen.
    South trace for GM footpoint; Output: lat, lon, arclen.
Magnetic field model:                          
    Internal: IGRF
    External: Tsyganenko 89C 
    External: Tsyganenko 89C     Kp:  3-,3,3+
    Stop trace altitude (km):   100.00
Formats and units:                          
    Day/Time format: YYYY DDD HH:MM
    Degrees/Hemisphere format: Decimal degrees with 2 place(s).
        Longitude 0 to 360, latitude -90 to 90.
    Distance format: Earth radii with 2 place(s).
Modification History
Originated 03/14/96
 
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FAST_TEAMS_PA_L2
Description
No TEXT global attribute value.
 
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FA_ESA_L2_EEB doi:10.48322/m36d-wr84
Description
ESA>Electrostatic Analyzer
Modification History
Rev-2 2021-09-28
 
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FA_ESA_L2_EES doi:10.48322/0ydx-j139
Description
ESA>Electrostatic Analyzer
Modification History
Rev-2 2021-09-28
 
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FA_ESA_L2_IEB doi:10.48322/3chd-sj41
Description
ESA>Electrostatic Analyzer
Modification History
Rev-2 2021-09-28
 
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FA_ESA_L2_IES doi:10.48322/9t9w-1q28
Description
ESA>Electrostatic Analyzer
Modification History
Rev-2 2021-09-28
 
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FA_K0_ACF doi:10.48322/23b9-6g23
Description
none yet
Modification History
none yet
 
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FA_K0_TMS doi:10.48322/78b7-gk94
Description
The Time-of-Flight Energy, Angle, Mass Spectrograph 
(TEAMS) Experiment for FAST,  D. M. Klumpar, E. Moebius, 
L. M. Kistler, M. Popecki, E. G. Shelley, E. Hertzberg, 
K. Crocker, M. Granoff, Li Tang, C. W. Carlson, 
J. McFadden, B. Klecker, F. Eberl, E. Kuenneth, 
H. Kaestle, M. Ertl, W. K. Peterson, and D. Hovestadt, 
published, Space Science Reviews, 
2001, volume 98, pages 197-291,  doi:10.1023/A:1013127607414. 
The 3-D Plasma Distribution Function Analyzers with 
Time-of-Flight Mass Discrimination for CLUSTER, FAST,and Equator-S, 
E. Moebius, L. M. Kistler, M. Popecki, 
K. Crocker, M. Granoff, Y. Jiang, E. Satori, V. Ye, 
H. Reme, J. A. Sauvaud, A. Cros, A. Aoustin, T. Camus, 
J. L. Medale, J. Rouzaud, C. W. Carlson, J. McFadden, 
D. Curtis, H. Heetdirks, J. Croyle, C. Ingraham, 
E. G. Shelley, D. M. Klumpar, E. Hertzberg, B. Klecker, 
M. Ertl, F. Eberl, H. Kaestle, E. Kuenneth, 
P. Laeverenz, E. Seidenschwang, G. Parks, M. McCarthy, 
A. Korth, B. Graeve, H. Balsiger, U. Schwab, and 
M. Steinacher, Measurement Techniques for Space 
Plasmas: Particles, 1998, Geophysical Monograph Series, 
volume 102, pages 243-248.
Data are derived from a time-of-flight mass spectrograph 
that determines 3-dimensional distribution functions of 
individual ion species over the energy range 1 - 12000 eV, 
within 2.5 seconds (one-half spacecraft spin).  The 
instrument consists of a toroidal top-hat electrostatic 
analyzer with instantaneous acceptance of ions over 360 
degrees in polar angle in 16 sectors.  Ions passing 
through the electrostatic analyzer are postaccelerated by 
up to 25 kV and then analyzed for mass per charge in a 
foil-based time-of-flight analyzer.  The data used to 
construct CDF data products are derived from the Survey 
data.  Survey data consists of 
4 mass groups x 48 energies x 64 solid angle segments. 
The 4 mass groups are H+, O+, He+, and He++.  Only the 
16 equatorial angle segments are used for the CDF data set. 
Each equatorial solid angle segment contains 2 (4) samples 
at each energy in the 32 (64) sweep/spin mode.  The full 
angular range is covered in half a spin but the actual 
time resolution of the survey data product depends upon 
the telemetry mode.  In the highest TM rate modes H+ and O+ 
survey data read out every half spin.  In lowest TM rate 
mode these data are accumulated for 4 spins.  The minimum 
accumulation time included in the CDF is 1 spin, so if the 
actual accumulation time is a half spin, two data points 
are averaged.  Otherwise, the full resolution is included. 
In every mode He+ and He++ are accumulated twice as long 
as H+ and O+.  To force the H+, O+, and He+ to have an 
equal number of data points when H+ and O+ have twice the 
time resolution, each He+ data point is written twice 
consecutively in the file. 
Modification History
none yet
 
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FM_K0_KILP (spase://GBO/NumericalData/FMI/Kilpisjarvi/AllSkyCamera/K0/PT1M)
Description
Keograms are quick-look data of an all-sky camera at 
Kilpisjarvi (69.02 N, 20.79 E)  
 maintained and operated by the Finnish Meteorological Institute.
Keograms show the intensity along the middle meridian of the camera 
field-of-view as a function of time. The camera has a fish-eye lens 
of 180 degrees and narrow bandpass interference filters of wavelengths 
557.7 nm (green) and 630.0 nm (red). In standard operating mode, the sampling
interval 
is 20 s and 60 s for the red and green images, respectively.
The exposure time is typically 1000 ms. The time resolution of keograms 
is 1 min and they are constructed using only the green images.
The size of a digital image is 512x512 pixels and intensity values 
vary between 0 and 255. At the altitude of 110 km the field-of-view 
(with reasonable spatial resolution) is a spherical area with the 
diameter of 600 km.  The keograms shown here are intensity versus latitude 
plots while the original keograms (available in http://www.geo.fmi.fi/MIRACLE 
are intensity versus zenith angle plots.
The conversion from zenith angle dependence to equidistant latitude grid 
causes occasionally artificial two-band structure to the keograms
(light bands below and above the darker zenith).
The artefact becomes visible especially during quiet periods, 
and the autoscaling color palette may even strengthen the effect.
Note that some keograms show also the Moon as a sphere or ellipsoid with 
very high, even saturating intensities. 
Modification History
CDF created 25.04.2001 06:34:32 UTC
 
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FORMOSAT5_AIP_IDN
Description
IDN>Ion Number Density. Advanced Ionospheric Probe (AIP) is provided by Graduate
Institute of Space Science, National Central University (NCU) for the FORMOSAT-5
satellite as a scientific payload. The AIP is an all-in-one plasma sensor with
sampling rate up to 8,192 Hz to measure ionospheric plasma concentrations,
velocities, and temperatures over a wide range of spatial scales. Once a
comprehensive dataset is available from the AIP, a systematic examination of
longitudinal and seasonal variations of the ionospheric parameters in the
topside F region can be conducted for all latitudinal coverage. The transient
and long-term variations of ionospheric plasma can be monitored in the upcoming
solar maximum period and are beneficial to predict the trend of the space
weather as well as the seismic precursors associated with earthquakes.
 
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G0_K0_EP8 (spase://NOAA/NumericalData/GOES/10/SEM/PT300S)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS)
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The energetic particle fluxes are 
 given as five-minute averaged values
 and the vector magnetic field is given
 as one-minute average values.
Flux values for three integral electron
 channels (E >0.6 MeV, E >2.0 MeV,
 and E >4.0 MeV) and one differential
 proton channel(0.7 MeV < E <4 MeV)
 are provided. These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94,
 GOES-9 launched on 5/23/95, and
 GOES-10 launched on 4/25/97. Typically
 two satellites are maintained
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Instrument data quality flags are set
 from real-time telemetry, or, in
 the case of historically-processed
 data sets when telemetry is not
 available, fixed to a level-1
 instrument status flag for all data
Reference: Geostationary Operational
 Environmental Satellite GOES I-M
 System Description, compiled by John
 Savides, Space Systems/Loral, Palo
 Alto, California, December 1992.
 Dr. Terrance Onsager, NOAA/SEC,
 tonsager@sec.noaa.gov, 303-497-5713,
 Boulder CO 80303 USA,
 or Martin Black, NOAA/SEC,
 mblack@sec.noaa.gov, 303-497-7235,
 325 Broadway, Boulder CO 80303 USA
NOTICE: GOES 12 energetic particle data are not available
due to the failure of two proton channels in the detectors.  These
 channels were used for the correction and processing of the proton 
and electron data.  Beginning April 8, 2003, the GOES energetic
 particle data are obtained from GOES 10 only. 
Modification History
 Version 2.0: 1st operational version,-db, 14 Jul 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.  -db, 16 Feb 93
 Added unit_ptr to s/c position units fixed CATDES on SC_pos_sm, fixed GSn  
-db, 20 Apr 93
Version 3.0: Major re-write, added  GOES-8 and GOES-9, -db 22 Feb 96.
Fixed 1-character xyz label problem,
   -db, 8 May 96
Minor text & label changes,
   -db, 29 Jul 96
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for EPS for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch date and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, and changed
CATDESC values for position variables from s/c to GOES 10. for GSE and GSM mag
field vectors. These changes were requested by Mona Kessel. -mblack, 12 Apr 1999
 
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G0_K0_GIFWALK
Description
Pre-generated PWG plots
 
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G0_K0_MAG (spase://NOAA/NumericalData/GOES/10/MAG/PT1M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS) and
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The vector magnetic field is 
 given as one-minute averaged values
 in three coordinate systems:
 (1) Spacecraft (s/c) P,E,N,
 (2) GSM x,y,z, (3) GSE x,y,z
s/c mag. field is defined as:
 Hp, perpendicular to the satellite
 orbital plane or parallel to the
 Earths spin axis in the case of
 a zero degree inclination orbit;
 He, perpendicular to Hp and
 directed earthwards; and
 Hn, perpendicular to both Hp and
 directed eastwards.
These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94,
 GOES-9 launched on 5/23/95, and
 GOES-10 launched on 4/25/97.
Typically two satellites are
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
 However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Instrument data quality flags are set
 from real-time telemetry, or, in
 the case of historically-processed
 data sets when telemetry is not
 available, fixed to a level-1
 instrument status flag for all data
Reference: Monitoring Space
 Weather with GOES Magnetometers,
 Singer, H.J, L. Matheson, R.Grubb
 A.Newman, and S.D.Bouwer, SPIE
 Proceedings, Volume 2812,
 4-9 Aug 1996.  For more info, contact:
Dr. Howard Singer, NOAA/SEC,
 hsinger@sec.noaa.gov, 303-497-6959,
 Boulder CO 80303 USA,
 or Martin Black, NOAA/SEC,
 mblack@sec.noaa.gov, 303-497-7235,
 325 Broadway, Boulder CO 80303 USA
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Version 3.0, Major re-write of text, 
 corrected label_1 bug (now cartesian),
 added GOES-8 & 9 CDFs,-db,26 Jan 1996
 Corrected no. of elements on lines 
   477-479 (labels), -db 7 May 1996
 Minor text changes, -db 22 Jul 1996
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for MAG for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch data and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, changed CATDESC
values for position variables from s/c to GOES 10, and added cartesian to
CATDESC for GSE and GSM mag field vectors. These changes were requested by Mona
Kessel. -mblack, 12 Apr 1999
 
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G10_L2_MAG (spase://NOAA/NumericalData/GOES/10/MAG/PT0.512S)
Description
Satellite positions and velocities derived from SSCWEB GEI ephemeris,
interpolated to one minute time resolution; perpendicular vectors for ENP
coordinate system derived from pos X vel. B field vectors in LH-ENP and GEI
systems, B field total magnitude, magnetotorquer counts, and data quality flags
derived from 512 msec binary GOES data files. 
General Comments from Dr. Howard J. Singer (GOES Magnetometer PI)  
 1. Data Description: A full description of the GOES magnetometer data,
including use of the quality flags and torquer current information, is contained
in a GOES 8-12 Magnetometer Readme File prepared by Dr. Howard J. Singer. The
GOES data have been prepared at NOAA Space Weather Prediction Center (SWPC) by
Dr. Howard J. Singer with major data processing and data evaluation
contributions by SWPC staff, Lorne Matheson and Ann Newman, as well as
coordinate transformation development by Dr. Paul Loto aniu (University of
Colorado/SWPC).
 2. Coordinate description for PEN: .Hp:  magnetic field vector component,
points northward, perpendicular to orbit plane which for a zero degree
inclination orbit is parallel to Earth's spin axis. .He:  magnetic field vector
component, perpendicular to Hp and Hn and points earthward. .Hn:  magnetic field
vector component, perpendicular to Hp and He and points eastward. Ht:  total
field. 
 3. Magnetometer offsets and noise: GOES 8-12 spacecraft are 3-axis stabilized.
There is only one opportunity for a spin maneuver at the beginning of the
mission to determine on-orbit magnetic field offsets. There are additional
complications that result from needing to know the changing offsets introduced
by torquer coils on the satellites. While comparisons of GOES data to model
fields during quiet times and comparisons to nearby encounters with other
spacecraft are used to demonstrate the observed data values are reasonable,
caution should be used in assigning absolute accuracy. While there has been a
significant effort to remove the effects of torquer coil interference in the
0.512 s data, there can be small, typically less than 1 nT spikes in the data at
the time of torquer current changes. More information on this topic is included
the more extensive readme file. This file is a living document that will be
updated periodically.  
4.  Orbital Inclination: During the primary operational lifetime of the GOES
satellites, the satellite inclination is typically kept within a few tenths of a
degree of 0 degrees inclination; however, as the satellite ages, the inclination
can grow to several degrees.
Modification History
Rev- 2008-11-03
 
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G11_L2_MAG (spase://NOAA/NumericalData/GOES/11/MAG/PT0.512S)
Description
Satellite positions and velocities derived from SSCWEB GEI ephemeris,
interpolated to one minute time resolution; perpendicular vectors for ENP
coordinate system derived from pos X vel. B field vectors in LH-ENP and GEI
systems, B field total magnitude, magnetotorquer counts, and data quality flags
derived from 512 msec binary GOES data files. 
General Comments from Dr. Howard J. Singer (GOES Magnetometer PI)  
 1. Data Description: A full description of the GOES magnetometer data,
including use of the quality flags and torquer current information, is contained
in a GOES 8-12 Magnetometer Readme File prepared by Dr. Howard J. Singer. The
GOES data have been prepared at NOAA Space Weather Prediction Center (SWPC) by
Dr. Howard J. Singer with major data processing and data evaluation
contributions by SWPC staff, Lorne Matheson and Ann Newman, as well as
coordinate transformation development by Dr. Paul Loto aniu (University of
Colorado/SWPC).
 2. Coordinate description for PEN: .Hp:  magnetic field vector component,
points northward, perpendicular to orbit plane which for a zero degree
inclination orbit is parallel to Earth's spin axis. .He:  magnetic field vector
component, perpendicular to Hp and Hn and points earthward. .Hn:  magnetic field
vector component, perpendicular to Hp and He and points eastward. Ht:  total
field. 
 3. Magnetometer offsets and noise: GOES 8-12 spacecraft are 3-axis stabilized.
There is only one opportunity for a spin maneuver at the beginning of the
mission to determine on-orbit magnetic field offsets. There are additional
complications that result from needing to know the changing offsets introduced
by torquer coils on the satellites. While comparisons of GOES data to model
fields during quiet times and comparisons to nearby encounters with other
spacecraft are used to demonstrate the observed data values are reasonable,
caution should be used in assigning absolute accuracy. While there has been a
significant effort to remove the effects of torquer coil interference in the
0.512 s data, there can be small, typically less than 1 nT spikes in the data at
the time of torquer current changes. More information on this topic is included
the more extensive readme file. This file is a living document that will be
updated periodically.  
4.  Orbital Inclination: During the primary operational lifetime of the GOES
satellites, the satellite inclination is typically kept within a few tenths of a
degree of 0 degrees inclination; however, as the satellite ages, the inclination
can grow to several degrees.
Modification History
Rev- 2008-11-03
 
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G12_L2_MAG (spase://NOAA/NumericalData/GOES/12/MAG/PT0.512S)
Description
Satellite positions and velocities derived from SSCWEB GEI ephemeris,
interpolated to one minute time resolution; perpendicular vectors for ENP
coordinate system derived from pos X vel. B field vectors in LH-ENP and GEI
systems, B field total magnitude, magnetotorquer counts, and data quality flags
derived from 512 msec binary GOES data files. 
General Comments from Dr. Howard J. Singer (GOES Magnetometer PI)  
 1. Data Description: A full description of the GOES magnetometer data,
including use of the quality flags and torquer current information, is contained
in a GOES 8-12 Magnetometer Readme File prepared by Dr. Howard J. Singer. The
GOES data have been prepared at NOAA Space Weather Prediction Center (SWPC) by
Dr. Howard J. Singer with major data processing and data evaluation
contributions by SWPC staff, Lorne Matheson and Ann Newman, as well as
coordinate transformation development by Dr. Paul Loto aniu (University of
Colorado/SWPC).
 2. Coordinate description for PEN: .Hp:  magnetic field vector component,
points northward, perpendicular to orbit plane which for a zero degree
inclination orbit is parallel to Earth's spin axis. .He:  magnetic field vector
component, perpendicular to Hp and Hn and points earthward. .Hn:  magnetic field
vector component, perpendicular to Hp and He and points eastward. Ht:  total
field. 
 3. Magnetometer offsets and noise: GOES 8-12 spacecraft are 3-axis stabilized.
There is only one opportunity for a spin maneuver at the beginning of the
mission to determine on-orbit magnetic field offsets. There are additional
complications that result from needing to know the changing offsets introduced
by torquer coils on the satellites. While comparisons of GOES data to model
fields during quiet times and comparisons to nearby encounters with other
spacecraft are used to demonstrate the observed data values are reasonable,
caution should be used in assigning absolute accuracy. While there has been a
significant effort to remove the effects of torquer coil interference in the
0.512 s data, there can be small, typically less than 1 nT spikes in the data at
the time of torquer current changes. More information on this topic is included
the more extensive readme file. This file is a living document that will be
updated periodically.  
4.  Orbital Inclination: During the primary operational lifetime of the GOES
satellites, the satellite inclination is typically kept within a few tenths of a
degree of 0 degrees inclination; however, as the satellite ages, the inclination
can grow to several degrees.
Modification History
Rev- 2008-11-03
 
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G6_K0_EPS (spase://NOAA/NumericalData/GOES/6/EPM/PT5M)
Description
The NOAA GOES satellites include 2 sensors: an Energetic Particle Sensor (EPS),
and a Magnetometer (MAG).
The satellites are geostationary. For older satellites, inclination may be up to
15 deg.
Data sometimes contains errors. especially GOES-6 EPS & possibly both  GOES 6,7
magnetometers. 
The EPS data are 5-min. averages, the MAG data are 1-min. averages. 
The NOAA Space Environment Lab (SEL), Space Environ. Services Center (SESC) uses
this data in real time for forecasting and monitoring. 
Reference: GOES Spacecraft OperationsManual, Volume I, May 1980, Hughes RefNo.
D5150 SCG 00169R
GOES-8, with 3 electron sensors should launch in early 93: the IE variables will
be defined post-launch.
For additional info., contact Dave Bouwer, NOAA/SEL, Mail Code R/E/SE, 325
Broadway, Boulder, CO 80303 USA (303)497-3899.
SELVAX::DBOUWER or dbouwer@selvax.sel.bldrdoc.gov
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Zeroed E1 electron channel - Instrument is far too damaged by radiation,   -db,
4 Jan 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.   -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn 
ADID_ref from 96 to 97   -db, 20 Apr 93
 
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G6_K0_MAG (spase://NOAA/NumericalData/GOES/6/MAG/PT60S)
Description
The NOAA GOES satellites include 2 sensors: an Energetic Particle Sensor (EPS),
and a Magnetometer (MAG).
The satellites are geostationary. For older satellites, inclination may be up to
15 deg.
Data sometimes contains errors.
The EPS data are 5-min. averages, the MAG data are 1-min. averages. 
B s/c has undeterm. errors in x,y B field for GSM and GSE is missing while
corrections are developed.
The NOAA Space Environment Lab (SEL), Space Environ. Services Center (SESC) uses
this data in real time for forecasting and monitoring. 
Reference: GOES Spacecraft OperationsManual, Volume I, May 1980, Hughes RefNo.
D5150 SCG 00169R
GOES-8, with 3 electron sensors should launch in early 93: the IE variables will
be defined post-launch.
For additional info., contact Dave Bouwer, NOAA/SEL, Mail Code R/E/SE, 325
Broadway, Boulder, CO 80303 USA (303)497-3899.
SELVAX::DBOUWER or dbouwer@selvax.sel.bldrdoc.gov
Modification History
 Version 2.0: 1st operational version,  -db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions.   -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 
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G7_K0_EPS (spase://NOAA/NumericalData/GOES/7/EPM/PT5M)
Description
The NOAA GOES satellites include 2 sensors: an Energetic Particle Sensor (EPS),
and a Magnetometer (MAG).
The satellites are geostationary. For older satellites, inclination may be up to
15 deg.
Data sometimes contains errors. especially GOES-6 EPS & possibly both  GOES 6,7
magnetometers. 
The EPS data are 5-min. averages, the MAG data are 1-min. averages. 
The NOAA Space Environment Lab (SEL), Space Environ. Services Center (SESC) uses
this data in real time for forecasting and monitoring. 
Reference: GOES Spacecraft OperationsManual, Volume I, May 1980, Hughes RefNo.
D5150 SCG 00169R
GOES-8, with 3 electron sensors should launch in early 93: the IE variables will
be defined post-launch.
For additional info., contact Dave Bouwer, NOAA/SEL, Mail Code R/E/SE, 325
Broadway, Boulder, CO 80303 USA (303)497-3899.
SELVAX::DBOUWER or dbouwer@selvax.sel.bldrdoc.gov
Modification History
 Version 2.0: 1st operational version,-db, 14 Jul 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.  -db, 16 Feb 93
 Added unit_ptr to s/c position units fixed CATDES on SC_pos_sm, fixed GSn  
-db, 20 Apr 93
Version 3.0: Major re-write, added  GOES-8 and GOES-9.
 
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G7_K0_MAG (spase://NOAA/NumericalData/GOES/7/MAG/PT60S)
Description
The NOAA GOES satellites include 2 sensors: an Energetic Particle Sensor (EPS),
and a Magnetometer (MAG).
The satellites are geostationary. For older satellites, inclination may be up to
15 deg.
Data sometimes contains errors.
The EPS data are 5-min. averages, the MAG data are 1-min. averages. 
B s/c has undeterm. errors in x,y B field for GSM and GSE is missing while
corrections are developed.
The NOAA Space Environment Lab (SEL), Space Environ. Services Center (SESC) uses
this data in real time for forecasting and monitoring. 
Reference: GOES Spacecraft OperationsManual, Volume I, May 1980, Hughes RefNo.
D5150 SCG 00169R
GOES-8, with 3 electron sensors should launch in early 93: the IE variables will
be defined post-launch.
For additional info., contact Dave Bouwer, NOAA/SEL, Mail Code R/E/SE, 325
Broadway, Boulder, CO 80303 USA (303)497-3899.
SELVAX::DBOUWER or dbouwer@selvax.sel.bldrdoc.gov
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Modif. label_2 to reflect loss of G7  He, Hn s/c instrument.
 Version 3.0, Major re-write of text, 
 corrected label_1  bug (now cartesian),
 added GOES-8 & 9 CDFs,  -db, 26 Jan 1996
 
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G7_K1_MAG (spase://NOAA/NumericalData/GOES/7/MAG/PowerSpectralDensity/PT1M)
Description
The NOAA GOES satellites include 2 sensors: an Energetic Particle Sensor (EPS),
and a Magnetometer (MAG).
The satellites are geostationary. For older satellites, inclination may be up to
15 deg.
Data sometimes contains errors.
The EPS data are 5-min. averages, the MAG data are 1-min. averages. 
B s/c has undeterm. errors in x,y B field for GSM and GSE is missing while
corrections are developed.
The NOAA Space Environment Lab (SEL), Space Environ. Services Center (SESC) uses
this data in real time for forecasting and monitoring. 
Reference: GOES Spacecraft OperationsManual, Volume I, May 1980, Hughes RefNo.
D5150 SCG 00169R
GOES-8, with 3 electron sensors should launch in early 93: the IE variables will
be defined post-launch.
For additional info., contact Dave Bouwer, NOAA/SEL, Mail Code R/E/SE, 325
Broadway, Boulder, CO 80303 USA (303)497-3899.
SELVAX::DBOUWER or dbouwer@selvax.sel.bldrdoc.gov
Modification History
 Version 1.0: 1st operational version, RLK, July 2000
 
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G8_K0_EP8 (spase://NOAA/NumericalData/GOES/8/EPS/PT5M)
Description
The NOAA Geostationary Operational 
Environmental Satellite (GOES) key
parameters are obtained from the
Energetic Particle Sensor (EPS)
and the magnetometer (MAG).  The
key parameters are a subset of the 
data available from the GOES Space
Environment Monitor (SEM) instruments.
The energetic particle fluxes are 
given as five-minute averaged values
and the vector magnetic field is given
as one-minute average values.
Flux values for three integral electron
channels (E >0.6 MeV, E >2.0 MeV,
and E >4.0 MeV) and one differential
proton channel(0.7 MeV < E <4 MeV)
are provided. These data are used by
NOAA Space Environment Center (SEC)
for the real-time monitoring and
prediction of the conditions in the
Earth's space environment.  A new
series of GOES spacecraft began
with GOES-8 launched on 4/13/94 and
GOES-9 launched on 5/23/95. Typically
two satellites are maintained
operational,one at about 135 degrees
geographic west longitude and one at
about 75 degrees geographic west
longitude. The satellite inclination
is typically within a few tenths of a
degree of the geographic equator.
However, the satellites can be moved,
especially during the six months to
one year following launch, and the
inclination can increase after years
of satellite operation.
Reference: Geostationary Operational
Environmental Satellite GOES I-M
System Description, compiled by John
Savides, Space Systems/Loral, Palo
Alto, California, December 1992.
Dr. Terrance Onsager, NOAA/SEC,
tonsager@sec.noaa.gov, 303-497-5713,
Boulder CO 80303 USA,
or Dave Bouwer, NOAA/SEC,
dbouwer@sel.noaa.gov, 303-497-3899,
325 Broadway, Boulder CO 80303 USA
Modification History
 Version 2.0: 1st operational version,-db, 14 Jul 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.  -db, 16 Feb 93
 Added unit_ptr to s/c position units fixed CATDES on SC_pos_sm, fixed GSn  
-db, 20 Apr 93
Version 3.0: Major re-write, added  GOES-8 and GOES-9, -db 22 Feb 96.
Fixed 1-character xyz label problem,
   -db, 8 May 96
Minor text & label changes,
   -db, 29 Jul 96
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for EPS for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch date and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, and changed
CATDESC values for position variables from s/c to GOES 8. for GSE and GSM mag
field vectors. These changes were requested by Mona Kessel. -mblack, 12 Apr 1999
 
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G8_K0_MAG (spase://NOAA/NumericalData/GOES/8/MAG/PT1M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS) and
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The vector magnetic field is 
 given as one-minute averaged values
 in three coordinate systems:
 (1) Spacecraft (s/c) P,E,N,
 (2) GSM x,y,z, (3) GSE x,y,z
s/c mag. field is defined as:
 Hp, perpendicular to the satellite
 orbital plane or parallel to the
 Earths spin axis in the case of
 a zero degree inclination orbit;
 He, perpendicular to Hp and
 directed earthwards; and
 Hn, perpendicular to both Hp and
 directed eastwards.
These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94 and
 GOES-9 launched on 5/23/95.
Typically two satellites are
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
 However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Reference: Monitoring Space
 Weather with GOES Magnetometers,
 Singer, H.J, L. Matheson, R.Grubb
 A.Newman, and S.D.Bouwer, SPIE
 Proceedings, Volume 2812,
 4-9 Aug 1996.  For more info, contact:
Dr. Howard Singer, NOAA/SEC,
 hsinger@sec.noaa.gov, 303-497-6959,
 Boulder CO 80303 USA,
 or Dave Bouwer, NOAA/SEC,
 dbouwer@sec.noaa.gov, 303-497-3899,
 325 Broadway, Boulder CO 80303 USA
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Version 3.0, Major re-write of text, 
 corrected label_1 bug (now cartesian),
 added GOES-8 & 9 CDFs,-db,26 Jan 1996
 Corrected no. of elements on lines 
   477-479 (labels), -db 7 May 1996
 Minor text changes, -db 22 Jul 1996
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for MAG for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch data and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, changed CATDESC
values for position variables from s/c to GOES 8, and added cartesian to CATDESC
for GSE and GSM mag field vectors. These changes were requested by Mona Kessel.
-mblack, 12 Apr 1999
 
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G9_K0_EP8 (spase://NOAA/NumericalData/GOES/9/EPS/PT5M)
Description
The NOAA Geostationary Operational 
Environmental Satellite (GOES) key
parameters are obtained from the
Energetic Particle Sensor (EPS)
and the magnetometer (MAG).  The
key parameters are a subset of the 
data available from the GOES Space
Environment Monitor (SEM) instruments.
The energetic particle fluxes are 
given as five-minute averaged values
and the vector magnetic field is given
as one-minute average values.
Flux values for three integral electron
channels (E >0.6 MeV, E >2.0 MeV,
and E >4.0 MeV) and one differential
proton channel(0.7 MeV < E <4 MeV)
are provided. These data are used by
NOAA Space Environment Center (SEC)
for the real-time monitoring and
prediction of the conditions in the
Earth's space environment.  A new
series of GOES spacecraft began
with GOES-8 launched on 4/13/94 and
GOES-9 launched on 5/23/95. Typically
two satellites are maintained
operational,one at about 135 degrees
geographic west longitude and one at
about 75 degrees geographic west
longitude. The satellite inclination
is typically within a few tenths of a
degree of the geographic equator.
However, the satellites can be moved,
especially during the six months to
one year following launch, and the
inclination can increase after years
of satellite operation.
Reference: Geostationary Operational
Environmental Satellite GOES I-M
System Description, compiled by John
Savides, Space Systems/Loral, Palo
Alto, California, December 1992.
Dr. Terrance Onsager, NOAA/SEC,
tonsager@sec.noaa.gov, 303-497-5713,
Boulder CO 80303 USA,
or Dave Bouwer, NOAA/SEC,
dbouwer@sel.noaa.gov, 303-497-3899,
325 Broadway, Boulder CO 80303 USA
Modification History
 Version 2.0: 1st operational version,-db, 14 Jul 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.  -db, 16 Feb 93
 Added unit_ptr to s/c position units fixed CATDES on SC_pos_sm, fixed GSn  
-db, 20 Apr 93
Version 3.0: Major re-write, added  GOES-8 and GOES-9, -db 22 Feb 96.
Fixed 1-character xyz label problem,
   -db, 8 May 96
Minor text & label changes,
   -db, 29 Jul 96
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
 
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G9_K0_MAG (spase://NOAA/NumericalData/GOES/9/MAG/PT1M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS) and
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The vector magnetic field is 
 given as one-minute averaged values
 in three coordinate systems:
 (1) Spacecraft (s/c) P,E,N,
 (2) GSM x,y,z, (3) GSE x,y,z
s/c mag. field is defined as:
 Hp, perpendicular to the satellite
 orbital plane or parallel to the
 Earths spin axis in the case of
 a zero degree inclination orbit;
 He, perpendicular to Hp and
 directed earthwards; and
 Hn, perpendicular to both Hp and
 directed eastwards.
These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94 and
 GOES-9 launched on 5/23/95.
Typically two satellites are
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
 However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Reference: Monitoring Space
 Weather with GOES Magnetometers,
 Singer, H.J, L. Matheson, R.Grubb
 A.Newman, and S.D.Bouwer, SPIE
 Proceedings, Volume 2812,
 4-9 Aug 1996.  For more info, contact:
Dr. Howard Singer, NOAA/SEC,
 hsinger@sec.noaa.gov, 303-497-6959,
 Boulder CO 80303 USA,
 or Dave Bouwer, NOAA/SEC,
 dbouwer@sec.noaa.gov, 303-497-3899,
 325 Broadway, Boulder CO 80303 USA
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Version 3.0, Major re-write of text, 
 corrected label_1 bug (now cartesian),
 added GOES-8 & 9 CDFs,-db,26 Jan 1996
 Corrected no. of elements on lines 
   477-479 (labels), -db 7 May 1996
 Minor text changes, -db 22 Jul 1996
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
 
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GALILEO_HELIO1DAY_POSITION (spase://NASA/NumericalData/Galileo/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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GALILEO_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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GENESIS_3DL2_GIM doi:10.48322/wdvm-s118
Description
Fully processed Level 2 solar wind ion data at 2.5-min intervals including
proton density (/cc), temperature (K), velocity vectors (km/s) in GSE and RTN
systems, alpha/proton ratio, and flags for times of bi-directional electron
streaming. 
 
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GE_1MIN_MAG_PLASMA_SW_ONLY (spase://JAXA/NumericalData/Geotail/CPI-MGF/PT1M)
Description
Minute averaged definitiveinterplanetary parameters data
 
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GE_AT_DEF (spase://JAXA/NumericalData/Geotail/Ephemeris/Def_AT/PT10M)
Description
TBS
Modification History
6/13/91 - Original Implementation
9/18/91 - Modified for new attitude file format changes.  ICCR 881
2/11/92 - Used the variable name TIME and type CDF_INT4 and size 3 instead of 
EPOCH, CDF_EPOCH and 1 for the time tags.  CCR 490
6/1/92 - Added global attributes TITLE, PROJECT, DISCIPLINE, SOURCE_NAME, 
DATA_VERSION, and MODS; added variable attributes VALIDMIN, VALIDMAX, 
LABL_PTR_1, and MONOTON; added variables EPOCH and LABEL_TIME; 
changed variable name TIME to TIME_PB5.  CCR 1066
11/07/92 - use cdf variable Epoch and Time_PB5
6/8/93 - Added global attributes ADID_ref and Logical_file_id.  CCR 1092
7/5/94 - CCR ISTP 1852, updated CDHF skeleton to CDF standards - JT
9/20/94 - Added global attributes GCI_RA_ERR and GCI_DECL_ERR.  CCR 1932
11/7/94 - Merged CCR 1852 changes and corrected errors 
made in CCR 1852.  ICCR 1884
12/7/94 - Modified MODS and LABLAXIS to follow ISTP standards.  ICCR 1885
 
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GE_AT_PRE (spase://JAXA/NumericalData/Geotail/Ephemeris/Pre_AT/PT10M)
Description
TBS
Modification History
6/13/91 - Original Implementation
9/18/91 - Modified for new attitude file format changes.  ICCR 881
2/11/92 - Used the variable name TIME and type CDF_INT4 and size 3 instead of 
EPOCH, CDF_EPOCH and 1 for the time tags.  CCR 490
6/1/92 - Added global attributes TITLE, PROJECT, DISCIPLINE, SOURCE_NAME, 
DATA_VERSION, and MODS; added variable attributes VALIDMIN, VALIDMAX, 
LABL_PTR_1, and MONOTON; added variables EPOCH and LABEL_TIME; 
changed variable name TIME to TIME_PB5.  CCR 1066
11/07/92 - use cdf variable Epoch and Time_PB5
6/8/93 - Added global attributes ADID_ref and Logical_file_id.  CCR 1092
7/5/94 - CCR ISTP 1852, updated CDHF skeleton to CDF standards - JT
9/20/94 - Added global attributes GCI_RA_ERR and GCI_DECL_ERR.  CCR 1932
11/7/94 - Merged CCR 1852 changes and corrected errors 
made in CCR 1852.  ICCR 1884
12/7/94 - Modified MODS and LABLAXIS to follow ISTP standards.  ICCR 1885
 
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GE_EDA12SEC_LEP (spase://JAXA/NumericalData/Geotail/LEP/EDA/PT12S)
Description
Editor-A data are only acquired with the real-time operation in 
Usuda Deep Space Center (UDSC),Japan, while the Editor-B data 
are 24-hours continuouslyrecorded in the onboard tape recorders 
and are dumpedover the NASA/JPL Deep Space Network (DSN) stations
Please use the Editor-A LEP dataset prior to the Editor-B LEP 
dataset sinceplasma moments in the Editor-A data are more reliable. 
(Plasma moments inthe Editor-B are calculated onboard.)
The ion energy analyzer (LEP-EAi) has two energy scan mode: 
RAM-A (60eV to 40 keV) and RAM-B (5 keV to 40 keV). 
The energy scan mode is automatically selected onboard depending 
on the incoming ion fluxes. At present, only the plasma moments 
in the RAM-A mode are plotted (listed) for the LEP-EAi data. 
(The LEP-EAi moments are presented by the solid lines in the plot.)
The plasma moment data of the solar wind analyzer (LEP-SW) should be
used only qualitatively. The LEP-SW plasma moments are plotted 
(listed) when the energy scan mode of LEP-EAi is RAM-B. (The 
LEP-SW moments are presented by the dotted lines in the plot.) 
J.Geomag.Geoelectr.,46,669,1994
Modification History
Created by R. McGuire on 9/1/2003; Adapted from GE_K0_LEP
 
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GE_EDA3SEC_MGF (spase://JAXA/NumericalData/Geotail/MGF/EDA/PT3S)
Description
The Bz offset is still contained in the magnetic field data. The
magnitude of the Bz offset is about 0.5 nT (+-0.3 nT). The corrected
version of the magnetic field data will be published soon.
Kokubun et al., Geotail Prelaunch Report, ISAS, 58-70, 1992
Modification History
Created by S.-H. Chen on 6/18/97; Adapted from GE_FO_MGF
 
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GE_EDB12SEC_LEP (spase://JAXA/NumericalData/Geotail/LEP/EDB/PT12S)
Description
Editor-A data are only acquired with the real-time operation in 
Usuda Deep Space Center (UDSC),Japan, while the Editor-B data 
are 24-hours continuously recorded in the onboard tape recorders 
and are dumped over the NASA/JPL Deep Space Network (DSN) stations.
Please use the Editor-A LEP dataset prior to the Editor-B LEP 
dataset since plasma moments in the Editor-A data are more reliable.
(Plasma moments in the Editor-B are calculated onboard.)
The ion energy analyzer (LEP-EAi) has two energy scan modes:
 RAM-A (60eV to 40 keV) and RAM-B (5 keV to 40 keV). 
The energy scan mode is automatically selected onboard depending 
on the incoming ion fluxes. At present, only the plasma moments 
in the RAM-A mode are plotted (listed) for the LEP-EAi data. 
(The LEP-EAi moments are presented by the solid lines in the plot.)
The plasma moment data of the solar wind analyzer (LEP-SW) should 
be used only qualitatively. The LEP-SW plasma moments are plotted 
(listed) when the energy scan mode of LEP-EAi is RAM-B. 
(The LEP-SW moments are presented by the dotted lines in the plot.) 
J.Geomag.Geoelectr.,46,669, 1994
Modification History
Created by R. McGuire on 9/1/2003; Adapted from GE_K0_MGF
 
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GE_EDB3SEC_MGF (spase://JAXA/NumericalData/Geotail/MGF/EDB.PT3S)
Description
The Bz offset is still contained in the magnetic field data. The
magnitude of the Bz offset is about 0.5 nT (+-0.3 nT). The corrected
version of the magnetic field data will be published soon.
Kokubun et al., Geotail Prelaunch Report, ISAS, 58-70, 1992
Modification History
Created by S.-H. Chen on 6/18/97; Adapted from GE_FO_MGF
 
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GE_H0_CPI (spase://JAXA/NumericalData/Geotail/CPI/SWA/PT48S)
Description
Version 6 data processing replaced version 5 processing for data after March 10,
2006, when the CPI team started using 64 energy steps per spectrum instead of
the previously used 32 steps per spectrum.  The change was made to ensure that
even for very cold flows, the spectrum would have a sufficient number of
significant points to derive moments.  The change resulted in 96s spectra and
96s-resolution moments, vs. 48s previously.
 
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GE_HPAMOM_CPI (spase://JAXA/NumericalData/Geotail/CPI/HPA/PT64S)
Description
 GEOTAIL Prelaunch Report 
  April 1992, SES-TD-92-007SY 
 CPI/HPA  Hot Plasma Analyzer 
    High Time Resolution Moments 
       Ion Number density 
       Ion Average Temperature 
       Ion Bulk Flow Velocity 
       Electron Number Density 
       Electron Average Temperature 
 CPI Survey Data will be made available 
 via the World Wide Web as image files 
 for the mission operation periods in a 
 compressed time resolution for viewing 
 and/or downloading with a WWW browser 
 from the URL: 
     http://www-pi.physics.uiowa.edu/www/cpi/  
Modification History
First Delivery version, 29-JUL-1998
Final Delivery version, 17-AUG-1998
 
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GE_K0_CPI (spase://JAXA/NumericalData/Geotail/CPI/KeyParameter/PT64S)
Description
GEOTAIL Prelaunch Report
 April 1992, SES-TD-92-007SY
 CPI-SW Solar Wind Analyzer
   Key Parameters
      Ion number density
      Average proton energy
      Bulk flow velocity
 CPI-HP Hot Plasma Analyzer
   Key Parameters
      Ion number density
      Average proton energy
      Average electron energy
      Bulk flow velocity
      Plasma pressure
 CPI-IC Ion Composition Analyzer
   Key Parameters
      Principal Species
        H+
        He++
        He+
        O+
 CPI Survey Data will be made available
 via the World Wide Web as image files
 for the mission operation periods in a
 compressed time resolution for viewing
 and/or downloading with a WWW browser
 from the URL
 http://www-pi.physics.uiowa.edu/ 
SPDF/SPOF Supplementary Information and Notes: 
Modification History
First Delivery version, 7-OCT-1993
v2.0,  12-APR-94, RLD Changed dimensions to 3 and 2 at recommendation of
                      Mona Kessel. Jeff Love (CDFSUPPORT) helped clean up
                      dimension problems.
v2.1,  20-JUL-94, RLD Change VALIDMIN dates for CPI data to be 1 Oct 92.
                      Added items to TEXT field to include all KPs and
                      defined coordinate system used for velocities.
v2.2,  24-JAN-95, RLD Added some new comments to the description section.
v2.3,  19-MAY-95, RLD Added SW_V Z-component.
v2.31,  8-Jun-95, RLD Corrected dependent variables to differentiate
                      between CDF's 2-D size 2 & 3 (i.e., 2 &
                      3-dimensional velocities).
v2.4,  28-Sep-95, RLD Updated text & variable min/max values for consistency.
v2.41, 21-DEC-95, RLD Updated for KPGS v2.3 delivery. Official external
                      version of ST is now v04.
 
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GE_K0_EFD (spase://JAXA/NumericalData/Geotail/EFD/PT64S)
Description
Geotail Prelaunch Report, April 1992
The sensor providing data here (called EFD-P in report above) measures the
difference of electric potential between two electrodes (probes) immersed in the
plasma.
There are two sperical probes and two wire antennas each of which is extended by
50 meters from the satellite in its rotational plane.
 The two sperical probes are opposite each other (100 meters tip-to-tip) as are
the two wire antennas. The probe pairs are orthogonal to each other.
Diving the potential difference by the distance between the probes or the
centers of the conducting portion of the wire antennas gives the electric field
component along the probe extension.
The measurement of the electric field in the satellite rotational plane gives
the vector electric field when the electric field along the magnetic field is
much smaller than the perpendicular component.
Modification History
Version 1.0 Jan. 12, 1993
Modified on 7/18/94 and 7/29/94 by JT
Modified on 9/9/94 by JT - KPGS CCR 0039
 
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GE_K0_EPI (spase://JAXA/NumericalData/Geotail/EPIC/PT96S)
Description
EPIC Instrument Description: 
 A) Supra-Thermal Ion Composition Spectrometer (STICS) Subsystem: 
    1) Ion Head/Telescope Coverage 
       Apperature Width:  53.4 polar deg 
       Apperature Center: Spacecraft spin plane
 B) Ion Composition Spectrometer (ICS) Subsystem: 
    1) Ion Head Coverage 
       Apperature Width:  60.0 polar deg excluding center 16.0 deg 
       Apperature Center: Spacecraft spin plane
    2) Electron Detector Coverage 
       Apperature Width:  60.0 polar deg 
       Apperature Center: Spacecraft spin plane
    3) Caution 
       ICS Ion channels can change between two sets of energy pass 
       bands from record to record; consult the associated energy 
       information to determine what the current values are.
Anisotropy Calculation Qualification: 
 A) a1, a2, phi1 and phi2 are not
    calculated when the count rate
    is below a threshhold, currently
    8 counts/96 seconds.
Modification History
v1.0 19-Sep-1991
v1.3 11-Mar-1992
v2.0 13-Jan-1993 changes for Standards and Convensions v1.1
v3.0 25-May-1994 a) corrected PDiffI_S_Eminus    dimen variance FTFF -> TFFF
 b) changed LABL_PTR_1 to LABLAXIS    for 3 variables
 c) removed several DEPEND1 attributes d) corrected indexing for M8/P2
 e) corrected anisotropy min/max    values from [0,2pi] to
    [-pi,+pi] for phi1 and to    [-pi/2,+pi/2] for phi2
 f) changed ratio SCALETYP from    linear to log
 g) narrowed several SCALEMIN/MAX    ranges
v3.1 16-Sep-1994 a) shortened TEXT entries to max of     80 char
 b) removed several DEPEND0/1 attributes
 c) removed value for Logical_file_id    entry
 
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GE_K0_GIFWALK
Description
Pre-generated PWG plots
 
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GE_K0_LEP (spase://JAXA/NumericalData/Geotail/LEP/PT64S)
Description
J.Geomag.Geoelectr.,46,669,1994
Modification History
created Oct 1994
Modified by JT Oct. 28, 1994
 
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GE_K0_MGF (spase://JAXA/NumericalData/Geotail/MGF/PT64S)
Description
Kokubun et al., Geotail Prelaunch Report, ISAS, 58-70, 1992
Modification History
Created on 8/7/92, Modified on 1/25/93, 
Modified on 2/19/93, Modified on 3/8/93, 
Modified on 4/16/93, Modified on 7/18/94 by JT, 
2007 Jan.: Modified to use inner , magnetometer (SW version 3), Bob MacDowall.
 
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GE_K0_PWI (spase://JAXA/NumericalData/Geotail/PWI/KP/PT64S)
Description
Text description of the experiment need to be defined by the developer
Modification History
7/24/92
4/4/94
 
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GE_K0_SPHA (spase://JAXA/NumericalData/Geotail/Ephemeris/Spin_Phase_KP/PT10M)
Description
Geotail Prelaunch Report April 1992
Modification History
4/6/92 - Original Implementation, CCR 935
6/12/92 - Added global attributes TITLE, PROJECT, 
DISCIPLINE, SOURCE_NAME, DATA_VERSION, and MODS;
added variable attributes VALIDMIN, VALIDMAX, LABL_PTR_1, and MONOTON;
added variables EPOCH and LABEL_TIME; 
changed variable name TIME to TIME_PB5. CCR 935
9/23/92 - Changed descriptor value from SPAH to SPHA. ICCR 1387
2/22/93 - Changed VALIDMAX of FAULT. CCR 1361
6/10/93 - Added ADID_ref and Logical_file_id. CCR 1092
6/14/94 - CCR ISTP 1852, updated CDHF skeleton to CDF standards - JT
11/9/94 - Correct errors made in ccr 1852.  ICCR 1884
 
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GE_OR_DEF (spase://JAXA/NumericalData/Geotail/Ephemeris/PT10M)
Description
TBS
Modification History
Originated Monday, May 13, 1991
Modified June 13, 1991 for version 2.1
Modified October 2,1991 for new global attributes, incr sizes
Modified 11/11/91 Add sun vector, replace space id with support id
Modified 1992 Feb 11 to use the variable name TIME and type CDF_INT4 instead of 
EPOCH and CDF_EPOCH for the time tags CCR 490
Modified 6/2/92 add project, discipline, source_name, data_version, title, and 
mods to global section; add validmin, validmax, labl_ptr_1 and monoton 
attributes to some variables; put epoch time back in, rename time to 
time_pb5; add label_time to variables
Modified 11/07/92 to use Epoch and Time_PB5 variable name
Modified 6/2/93 add ADID_ref and Logical_file_id
7/5/94 - CCR ISTP 1852 updated CDHF skeleton to CDF standards - JT
9/21/94 - Added 24 new global attributes to log the ephemeris 
comparison summary report from the definitive FDF orbit file.  CCR 1932
11/7/94 - Merged CCR 1852 changes and corrected errors 
made in CCR 1852.  ICCR 1884
12/7/94 - Modified MODS to follow ISTP standards.  ICCR 1885
01/05/95 - add heliocentric coordinate system.  CCR 1889
2/28/95 - added COMMENT1 and COMMENT2 for CCR 
11/03/95 - deleted crn_space for CCR 2154 - RM
09/20/96 - changed CRN to CRN_EARTH for CCR 2269
 
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GE_OR_GIFWALK
Description
Pre-generated ISTP orbit plots
 
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GE_OR_PRE (spase://JAXA/NumericalData/Geotail/Ephemeris/PT600S)
Description
TBS
Modification History
Originated Monday, May 13, 1991
Modified June 13, 1991 for version 2.1
Modified October 2,1991 for new global attributes, incr sizes
Modified 11/11/91 Add sun vector, replace space id with support id
Modified 1992 Feb 11 to use the variable name TIME and type CDF_INT4 instead of 
EPOCH and CDF_EPOCH for the time tags CCR 490
Modified 6/2/92 add project, discipline, source_name, data_version, title, and 
mods to global section; add validmin, validmax, labl_ptr_1 and monoton 
attributes to some variables; put epoch time back in, rename time to 
time_pb5; add label_time to variables
Modified 11/07/92 to use Epoch and Time_PB5 variable name
Modified 6/2/93 add ADID_ref and Logical_file_id
7/5/94 - CCR ISTP 1852 updated CDHF skeleton to CDF standards - JT
9/21/94 - Added 24 new global attributes to log the ephemeris 
comparison summary report from the definitive FDF orbit file.  CCR 1932
11/7/94 - Merged CCR 1852 changes and corrected errors 
made in CCR 1852.  ICCR 1884
12/7/94 - Modified MODS to follow ISTP standards.  ICCR 1885
01/05/95 - add heliocentric coordinate system.  CCR 1889
2/28/95 - added COMMENT1 and COMMENT2 for CCR 
11/03/95 - deleted crn_space for CCR 2154 - RM
09/20/96 - changed CRN to CRN_EARTH for CCR 2269
 
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GE_SW_CPI (spase://JAXA/NumericalData/Geotail/CPI/SWMD/PT48S)
Description
No TEXT global attribute value.
 
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GIACOBINI_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/Giacobini/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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GIACOBINI_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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GIOTTO_HELIO1DAY_POSITION (spase://NASA/NumericalData/Giotto/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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GIOTTO_HELIO1HR_POSITION
Description
The hourly data are made by the linear interpolation of old daily files
 
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GOES10_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/10/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
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GOES11_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/11/Ephemeris/PT3M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
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GOES11_K0_EP8 (spase://NOAA/NumericalData/GOES/11/EPS/PT5M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS)
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The energetic particle fluxes are 
 given as five-minute averaged values
 and the vector magnetic field is given
 as one-minute average values.
Flux values for three integral electron
 channels (E >0.6 MeV, E >2.0 MeV,
 and E >4.0 MeV) and one differential
 proton channel(0.7 MeV < E <4 MeV)
 are provided. These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94,
 GOES-9 launched on 5/23/95,
 GOES-10 launched on 4/25/97,
 GOES-11 launched on 5/3/2000, and 
 GOES-12 launched on 7/23/2001.
 Typically two satellites are maintained
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Instrument data quality flags are set
 from real-time telemetry, or, in
 the case of historically-processed
 data sets when telemetry is not
 available, fixed to a level-1
 instrument status flag for all data
Reference: Geostationary Operational
 Environmental Satellite GOES I-M
 System Description, compiled by John
 Savides, Space Systems/Loral, Palo
 Alto, California, December 1992.
 Dr. Terrance Onsager, NOAA/SEC,
 Terry.Onsager@noaa.gov, 303-497-5713,
 325 Broadway, Boulder CO 80305 USA,
 or Ann Newman, NOAA/SEC,
 Ann.Newman@noaa.gov, 303-497-5100,
 325 Broadway, Boulder CO 80305 USA
Modification History
 Version 2.0: 1st operational version,-db, 14 Jul 92
 Corrected S/C location error & added Geographic (not geodetic) & GEO S/C
positions.  -db, 16 Feb 93
 Added unit_ptr to s/c position units fixed CATDES on SC_pos_sm, fixed GSn  
-db, 20 Apr 93
Version 3.0: Major re-write, added  GOES-8 and GOES-9, -db 22 Feb 96.
Fixed 1-character xyz label problem,
   -db, 8 May 96
Minor text & label changes,
   -db, 29 Jul 96
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for EPS for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch date and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, and changed
CATDESC values for position variables from s/c to GOES 11. for GSE and GSM mag
field vectors. These changes were requested by Mona Kessel. -mblack, 12 Apr 1999
Updated metadata with GOES-11 launch date and with a Logical_source value that
includes the word GOES. This is in preparation of GOES-11 replacing GOES-10 as
GOES West in late June, 2006 -anewman June 23, 2006
 
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GOES11_K0_MAG (spase://NOAA/NumericalData/GOES/11/MAG/PT1M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS) and
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The vector magnetic field is 
 given as one-minute averaged values
 in three coordinate systems:
 (1) Spacecraft (s/c) P,E,N,
 (2) GSM x,y,z, (3) GSE x,y,z
s/c mag. field is defined as:
 Hp, perpendicular to the satellite
 orbital plane or parallel to the
 Earths spin axis in the case of
 a zero degree inclination orbit;
 He, perpendicular to Hp and
 directed earthwards; and
 Hn, perpendicular to both Hp and
 directed eastwards.
These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94,
 GOES-9 launched on 5/23/95,
 GOES-10 launched on 4/25/97,
 GOES-11 launched on 5/3/2000, and
 GOES-12 launched on 7/23/2001.
Typically two satellites are
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
 However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Instrument data quality flags are set
 from real-time telemetry, or, in
 the case of historically-processed
 data sets when telemetry is not
 available, fixed to a level-1
 instrument status flag for all data
Reference: Monitoring Space
 Weather with GOES Magnetometers,
 Singer, H.J, L. Matheson, R.Grubb
 A.Newman, and S.D.Bouwer, SPIE
 Proceedings, Volume 2812,
 4-9 Aug 1996.  For more info, contact:
Dr. Howard Singer, NOAA/SEC,
 Howard.Singer@noaa.gov,303-497-6959
 325 Broadway,Boulder CO 80305 USA,
 or Ann Newman, NOAA/SEC,
 Ann.Newman@noaa.gov, 303-497-5100,
 325 Broadway, Boulder CO 80305 USA
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Version 3.0, Major re-write of text, 
 corrected label_1 bug (now cartesian),
 added GOES-8 & 9 CDFs,-db,26 Jan 1996
 Corrected no. of elements on lines 
   477-479 (labels), -db 7 May 1996
 Minor text changes, -db 22 Jul 1996
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for MAG for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch data and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, changed CATDESC
values for position variables from s/c to GOES 11, and added cartesian to
CATDESC for GSE and GSM mag field vectors. These changes were requested by Mona
Kessel. -mblack, 12 Apr 1999
Updated metadata with GOES-11 launch date and with a Logical_source value that
includes the word GOES. This is in preparation of GOES-11 replacing GOES-10 as
GOES West in late June, 2006 -anewman June 23, 2006
 
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GOES12_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/12/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
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GOES12_K0_MAG (spase://NOAA/NumericalData/GOES/12/MAG/PT1M)
Description
The NOAA Geostationary Operational 
 Environmental Satellite (GOES) key
 parameters are obtained from the
 Energetic Particle Sensor (EPS) and
 and the magnetometer (MAG).  The
 key parameters are a subset of the 
 data available from the GOES Space
 Environment Monitor (SEM) instruments.
The vector magnetic field is 
 given as one-minute averaged values
 in three coordinate systems:
 (1) Spacecraft (s/c) P,E,N,
 (2) GSM x,y,z, (3) GSE x,y,z
s/c mag. field is defined as:
 Hp, perpendicular to the satellite
 orbital plane or parallel to the
 Earths spin axis in the case of
 a zero degree inclination orbit;
 He, perpendicular to Hp and
 directed earthwards; and
 Hn, perpendicular to both Hp and
 directed eastwards.
These data are used by
 NOAA Space Environment Center (SEC)
 for the real-time monitoring and
 prediction of the conditions in the
 Earth's space environment.  A new
 series of GOES spacecraft began
 with GOES-8 launched on 4/13/94,
 GOES-9 launched on 5/23/95, and
 GOES-10 launched on 4/25/97.
Typically two satellites are
 operational,one at about 135 degrees
 geographic west longitude and one at
 about 75 degrees geographic west
 longitude. The satellite inclination
 is typically within a few tenths of a
 degree of the geographic equator.
 However, the satellites can be moved,
 especially during the six months to
 one year following launch, and the
 inclination can increase after years
 of satellite operation.
Instrument data quality flags are set
 from real-time telemetry, or, in
 the case of historically-processed
 data sets when telemetry is not
 available, fixed to a level-1
 instrument status flag for all data
Reference: Monitoring Space
 Weather with GOES Magnetometers,
 Singer, H.J, L. Matheson, R.Grubb
 A.Newman, and S.D.Bouwer, SPIE
 Proceedings, Volume 2812,
 4-9 Aug 1996.  For more info, contact:
Dr. Howard Singer, NOAA/SEC,
 Howard.Singer@noaa.gov,303-497-6959
 325 Broadway,Boulder CO 80305 USA,
 or Ann Newman, NOAA/SEC,
 Ann.Newman@noaa.gov, 303-497-5100,
 325 Broadway, Boulder CO 80305 USA
Modification History
 Version 2.0: 1st operational version,-db, 15 Dec 92
 Corrected S/C location error & added  Geographic (not geodetic) & GEO S/C 
positions 
 Fixed ADID_ref from 97 to 96    -db, 16 Feb 93
 Added unit_ptr to s/c position units, fixed CATDES on SC_pos_sm, fixed GSn   
-db, 27 Apr 93
 Version 3.0, Major re-write of text, 
 corrected label_1 bug (now cartesian),
 added GOES-8 & 9 CDFs,-db,26 Jan 1996
 Corrected no. of elements on lines 
   477-479 (labels), -db 7 May 1996
 Minor text changes, -db 22 Jul 1996
Added global metadata, support_data  text, blank variable attrib. data  per Mona
Kessel sample file, -db, 5 Aug 96 
Added xyz GEO,GSE,GSM labels, 
 replacing 1 cartesian label  -db, 29 Aug 96 
Create 1 skeleton table for MAG for all GOES  preparing for the switch from
GOES-9 to 10  -anewman, 22 Jul 1998 
Added GOES-10 launch data and replaced Ann Newman with Martin Black as contact
person. -mblack, 18 Mar 1999 
Changed Epoch and Time_PB5 VAR_TYPEs from data to support_data, changed CATDESC
values for position variables from s/c to GOES 12, and added cartesian to
CATDESC for GSE and GSM mag field vectors. These changes were requested by Mona
Kessel. -mblack, 12 Apr 1999
Updated metadata with GOES-11 launch date and with a Logical_source value that
includes the word GOES. This is in preparation of GOES-11 replacing GOES-10 as
GOES West in late June, 2006 -anewman June 23, 2006
 
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GOES13_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN (spase://NOAA/NumericalData/GOES/13/EPS/EPEAD/E13EW/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS:integral electron flux corrected and flagged using complete set
of Sauer coefficients and flagged when data are bad due to solar proton
contamination; channel E3 not included in this version.
 
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GOES13_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/13/Ephemeris/PT3M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
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GOES13_EPS-MAGED_1MIN (spase://NOAA/NumericalData/GOES/13/EPS/MAGED/19ME15/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
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GOES13_EPS-MAGED_5MIN (spase://NOAA/NumericalData/GOES/13/EPS/MAGED/19ME15/PT5M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
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GOES13_EPS-PITCH-ANGLES_1MIN (spase://NOAA/NumericalData/GOES/13/EPS/SEM/L2/PitchAngle/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
 
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Data Access Code Examples written in Python and IDL®.
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GOES14_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN (spase://NOAA/NumericalData/GOES/14/EPS/EPEAD/E13EW/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS:integral electron flux corrected and flagged using complete set
of Sauer coefficients and flagged when data are bad due to solar proton
contamination; channel E3 not included in this version.
 
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Data Access Code Examples written in Python and IDL®.
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GOES14_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/14/Ephemeris/PT3M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES14_EPS-MAGED_1MIN (spase://NOAA/NumericalData/GOES/14/EPS/MAGED/19ME15/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES14_EPS-MAGED_5MIN (spase://NOAA/NumericalData/GOES/14/EPS/MAGED/19ME15/PT5M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES14_EPS-PITCH-ANGLES_1MIN (spase://NOAA/NumericalData/GOES/14/EPS/SEM/L2/PitchAngle/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES15_EPEAD-SCIENCE-ELECTRONS-E13EW_1MIN (spase://NOAA/NumericalData/GOES/15/EPS/EPEAD/E13EW/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS:integral electron flux corrected and flagged using complete set
of Sauer coefficients and flagged when data are bad due to solar proton
contamination; channel E3 not included in this version.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES15_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/15/Ephemeris/PT3M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES15_EPS-MAGED_1MIN (spase://NOAA/NumericalData/GOES/15/EPS/MAGED/19ME15/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES15_EPS-MAGED_5MIN (spase://NOAA/NumericalData/GOES/15/EPS/MAGED/19ME15/PT5M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
Modification History
Final release updates 8/23/2013 REM
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES15_EPS-PITCH-ANGLES_1MIN (spase://NOAA/NumericalData/GOES/15/EPS/SEM/L2/PitchAngle/PT1M)
Description
Data has been recast from original NOAA netCDF files by SPDF. DATA
CAVEATS/WARNINGS: The MagED data may not be accurate at times due to instrument
limitations such as dead time and proton contamination. Every effort is made to
reduce these effects but uncertainties are inevitable. Additionally, the
detectors may suffer from intermittent noise problems. Please contact Juan V.
Rodriguez (sem.goes@noaa.gov) with questions or concerns.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES16_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/16/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES17_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/17/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES18_EPHEMERIS_SSC
Description
Data quantities are generated from the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES8_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/8/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOES9_EPHEMERIS_SSC (spase://NOAA/NumericalData/GOES/9/Ephemeris/PT1M)
Description
Data quantities are generated fromt the SSCWeb system
Modification History
Originated 03/14/96
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GOLD_L2_NMAX (spase://NASA/NumericalData/GOLD/L2/NMAX/PT900S)
Description
The GOLD mission of opportunity flies an ultraviolet (UV) imaging spectrograph
on a geostationary satellite to measure densities and temperatures in Earth's
thermosphere and ionosphere and to understand the global-scale response to
forcing in the integrate Sun-Earth system. Visit 'https://gold.cs.ucf.edu' for 
more details.
 
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GOLD_L2_O2DEN
Description
The GOLD mission of opportunity flies an ultraviolet (UV) imaging spectrograph
on a geostationary satellite to measure densities and temperatures in Earth's
thermosphere and ionosphere and to understand the global-scale response to
forcing in the integrate Sun-Earth system. Visit 'https://gold.cs.ucf.edu' for 
more details.
 
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GOLD_L2_ON2 (spase://NASA/NumericalData/GOLD/L2/ON2/PT8S)
Description
The GOLD mission of opportunity flies an ultraviolet (UV) imaging spectrograph
on a geostationary satellite to measure densities and temperatures in Earth's
thermosphere and ionosphere and to understand the global-scale response to
forcing in the integrate Sun-Earth system. Visit 'https://gold.cs.ucf.edu' for 
more details.
 
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GOLD_L2_TDISK (spase://NASA/NumericalData/GOLD/L2/TDISK/PT8S)
Description
The GOLD mission of opportunity flies an ultraviolet (UV) imaging spectrograph
on a geostationary satellite to measure densities and temperatures in Earth's
thermosphere and ionosphere and to understand the global-scale response to
forcing in the integrate Sun-Earth system. Visit 'https://gold.cs.ucf.edu' for 
more details.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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GPS_RF_LANL-VTEC-1HR
Description
No TEXT global attribute value.
 
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GPS_ROTI15MIN_JPL doi:10.48322/v9pw-wd37
Description
The ROTI index is the standard deviation of the Rate of change of TEC (ROT)
during a 5-minute interval. TEC is the Total Electron Content measured between a
GPS satellite and ground receiver station.
 
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GPS_TEC15MIN_IGS (spase://NASA/NumericalData/IGS/GPS_Receiver/TEC/PT15M)
Description
The IGS global system of satellite tracking stations, Data Centers, and Analysis
Centers puts high-quality GPS data and data products on line in near real time
to meet the objectives of a wide range of scientific and engineering
applications and studies.  The IGS collects, archives, and distributes GPS
observation data sets of sufficient accuracy to satisfy the objectives of a wide
range of applications and experimentation.  These data sets are used by the IGS
to generate the data products mentioned above which are made available to
interested users through the Internet.  In particular, the accuracies of IGS
products are sufficient for the improvement and extension of the International
Terrestrial Reference Frame (ITRF), the monitoring of solid Earth deformations,
the monitoring of Earth rotation and variations in the liquid Earth (sea level,
ice-sheets, etc.), for scientific satellite orbit determinations, ionosphere
monitoring, and recovery of precipitable water vapor measurements.  
The primary mission of the International GPS Service, as stated in the
organization's 2002-2007 Strategic Plan, is 
    The International GPS Service is committed to providing the highest quality
data and products as the standard for global navigation satellite systems (GNSS)
in support of Earth science research, multidisciplinary applications, and
education. These activities aim to advance scientific understanding of the Earth
system components and their interactions, as well as to facilitate other
applications benefiting society.
The IGS Terms of Reference (comparable to the by-laws of the organization)
describes in broad terms the goals and organization of the IGS.  To accomplish
its mission, the IGS has a number of components: an international network of
over 350 continuously operating dual-frequency GPS stations, more than a dozen
regional and operational data centers, three global data centers, seven analysis
centers and a number of associate or regional analysis centers. The Central
Bureau for the service is located at the Jet Propulsion Laboratory, which
maintains the Central Bureau Information System (CBIS) and ensures access to IGS
products and information. An international Governing Board oversees all aspects
of the IGS.  The IGS is an approved service of the International Association of
Geodesy since 1994 and is recognized as a member of the Federation of
Astronomical and Geophysical Data Analysis Services (FAGS) since 1996. 
The IGS collects, archives, and distributes GPS observation data sets of
sufficient accuracy to meet the objectives of a wide range of scientific and
engineering applications and studies. These data sets are used to generate the
following products:
  * GPS satellite ephemerides
  * GLONASS satellite ephemerides
  * Earth rotation parameters
  * IGS tracking station coordinates and velocities
  * GPS satellite and IGS tracking station clock information
  * Zenith tropospheric path delay estimates
  * Global ionospheric maps
IGS products support scientific activities such as improving and extending the
International Earth Rotation Service (IERS) Terrestrial Reference Frame (ITRF),
monitoring deformations of the solid Earth and variations in the liquid Earth
(sea level, ice sheets, etc.), and in Earth rotation, determining orbits of
scientific satellites and monitoring the ionosphere. For example, geodynamics
investigators who use GPS in local regions can include data from one or more
nearby IGS stations, fix the site coordinates from such stations to their ITRF
values, and more importantly, use the precise IGS orbits without further
refinement. Data from an investigator's local network can then be analyzed with
maximum accuracy and minimum computational burden. Furthermore, the results will
be in a well-defined global reference frame.  An additional aspect of IGS
products is for the densification of the ITRF at a more regional level. This is
accomplished through the rigorous combination of regional or local network
solutions utilizing the Solution Independent Exchange Format (SINEX) and a
process defined in the densification section.  In the future, the IGS
infrastructure could become a valuable asset for support of new ground-based
applications -- and could also contribute to space-based missions in which
highly accurate flight and ground differential techniques are required.
 
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GPS_TEC1HR_IGS (spase://NASA/NumericalData/IGS/GPS_Receiver/TEC/PT60M)
Description
The IGS global system of satellite tracking stations, Data Centers, and Analysis
Centers puts high-quality GPS data and data products on line in near real time
to meet the objectives of a wide range of scientific and engineering
applications and studies.  The IGS collects, archives, and distributes GPS
observation data sets of sufficient accuracy to satisfy the objectives of a wide
range of applications and experimentation.  These data sets are used by the IGS
to generate the data products mentioned above which are made available to
interested users through the Internet.  In particular, the accuracies of IGS
products are sufficient for the improvement and extension of the International
Terrestrial Reference Frame (ITRF), the monitoring of solid Earth deformations,
the monitoring of Earth rotation and variations in the liquid Earth (sea level,
ice-sheets, etc.), for scientific satellite orbit determinations, ionosphere
monitoring, and recovery of precipitable water vapor measurements.  
The primary mission of the International GPS Service, as stated in the
organization's 2002-2007 Strategic Plan, is 
    The International GPS Service is committed to providing the highest quality
data and products as the standard for global navigation satellite systems (GNSS)
in support of Earth science research, multidisciplinary applications, and
education. These activities aim to advance scientific understanding of the Earth
system components and their interactions, as well as to facilitate other
applications benefiting society.
The IGS Terms of Reference (comparable to the by-laws of the organization)
describes in broad terms the goals and organization of the IGS.  To accomplish
its mission, the IGS has a number of components: an international network of
over 350 continuously operating dual-frequency GPS stations, more than a dozen
regional and operational data centers, three global data centers, seven analysis
centers and a number of associate or regional analysis centers. The Central
Bureau for the service is located at the Jet Propulsion Laboratory, which
maintains the Central Bureau Information System (CBIS) and ensures access to IGS
products and information. An international Governing Board oversees all aspects
of the IGS.  The IGS is an approved service of the International Association of
Geodesy since 1994 and is recognized as a member of the Federation of
Astronomical and Geophysical Data Analysis Services (FAGS) since 1996. 
The IGS collects, archives, and distributes GPS observation data sets of
sufficient accuracy to meet the objectives of a wide range of scientific and
engineering applications and studies. These data sets are used to generate the
following products:
  * GPS satellite ephemerides
  * GLONASS satellite ephemerides
  * Earth rotation parameters
  * IGS tracking station coordinates and velocities
  * GPS satellite and IGS tracking station clock information
  * Zenith tropospheric path delay estimates
  * Global ionospheric maps
IGS products support scientific activities such as improving and extending the
International Earth Rotation Service (IERS) Terrestrial Reference Frame (ITRF),
monitoring deformations of the solid Earth and variations in the liquid Earth
(sea level, ice sheets, etc.), and in Earth rotation, determining orbits of
scientific satellites and monitoring the ionosphere. For example, geodynamics
investigators who use GPS in local regions can include data from one or more
nearby IGS stations, fix the site coordinates from such stations to their ITRF
values, and more importantly, use the precise IGS orbits without further
refinement. Data from an investigator's local network can then be analyzed with
maximum accuracy and minimum computational burden. Furthermore, the results will
be in a well-defined global reference frame.  An additional aspect of IGS
products is for the densification of the ITRF at a more regional level. This is
accomplished through the rigorous combination of regional or local network
solutions utilizing the Solution Independent Exchange Format (SINEX) and a
process defined in the densification section.  In the future, the IGS
infrastructure could become a valuable asset for support of new ground-based
applications -- and could also contribute to space-based missions in which
highly accurate flight and ground differential techniques are required.
 
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GPS_TEC2HR_IGS (spase://NASA/NumericalData/IGS/GPS_Receiver/TEC/PT120M)
Description
The IGS global system of satellite tracking stations, Data Centers, and Analysis
Centers puts high-quality GPS data and data products on line in near real time
to meet the objectives of a wide range of scientific and engineering
applications and studies.  The IGS collects, archives, and distributes GPS
observation data sets of sufficient accuracy to satisfy the objectives of a wide
range of applications and experimentation.  These data sets are used by the IGS
to generate the data products mentioned above which are made available to
interested users through the Internet.  In particular, the accuracies of IGS
products are sufficient for the improvement and extension of the International
Terrestrial Reference Frame (ITRF), the monitoring of solid Earth deformations,
the monitoring of Earth rotation and variations in the liquid Earth (sea level,
ice-sheets, etc.), for scientific satellite orbit determinations, ionosphere
monitoring, and recovery of precipitable water vapor measurements.  
The primary mission of the International GPS Service, as stated in the
organization's 2002-2007 Strategic Plan, is 
    The International GPS Service is committed to providing the highest quality
data and products as the standard for global navigation satellite systems (GNSS)
in support of Earth science research, multidisciplinary applications, and
education. These activities aim to advance scientific understanding of the Earth
system components and their interactions, as well as to facilitate other
applications benefiting society.
The IGS Terms of Reference (comparable to the by-laws of the organization)
describes in broad terms the goals and organization of the IGS.  To accomplish
its mission, the IGS has a number of components: an international network of
over 350 continuously operating dual-frequency GPS stations, more than a dozen
regional and operational data centers, three global data centers, seven analysis
centers and a number of associate or regional analysis centers. The Central
Bureau for the service is located at the Jet Propulsion Laboratory, which
maintains the Central Bureau Information System (CBIS) and ensures access to IGS
products and information. An international Governing Board oversees all aspects
of the IGS.  The IGS is an approved service of the International Association of
Geodesy since 1994 and is recognized as a member of the Federation of
Astronomical and Geophysical Data Analysis Services (FAGS) since 1996. 
The IGS collects, archives, and distributes GPS observation data sets of
sufficient accuracy to meet the objectives of a wide range of scientific and
engineering applications and studies. These data sets are used to generate the
following products:
  * GPS satellite ephemerides
  * GLONASS satellite ephemerides
  * Earth rotation parameters
  * IGS tracking station coordinates and velocities
  * GPS satellite and IGS tracking station clock information
  * Zenith tropospheric path delay estimates
  * Global ionospheric maps
IGS products support scientific activities such as improving and extending the
International Earth Rotation Service (IERS) Terrestrial Reference Frame (ITRF),
monitoring deformations of the solid Earth and variations in the liquid Earth
(sea level, ice sheets, etc.), and in Earth rotation, determining orbits of
scientific satellites and monitoring the ionosphere. For example, geodynamics
investigators who use GPS in local regions can include data from one or more
nearby IGS stations, fix the site coordinates from such stations to their ITRF
values, and more importantly, use the precise IGS orbits without further
refinement. Data from an investigator's local network can then be analyzed with
maximum accuracy and minimum computational burden. Furthermore, the results will
be in a well-defined global reference frame.  An additional aspect of IGS
products is for the densification of the ITRF at a more regional level. This is
accomplished through the rigorous combination of regional or local network
solutions utilizing the Solution Independent Exchange Format (SINEX) and a
process defined in the densification section.  In the future, the IGS
infrastructure could become a valuable asset for support of new ground-based
applications -- and could also contribute to space-based missions in which
highly accurate flight and ground differential techniques are required.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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HALEBOPP_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/HaleBopp/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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HALEBOPP_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
Dataset in CDAWeb
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HALLEY_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/Halley/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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HALLEY_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
Dataset in CDAWeb
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HEL1_6SEC_NESSMAG doi:10.48322/nzxp-3e54
Description
This dataset contains high resolution interplanetary magnetic field data in
six-second averages as measured by the Helios 1 tri-axial fluxgate magnetometer
experiment. Magnetic field vector components in nanotelsa [nT] are given in
solar-ecliptic (SE) spacecraft-centered coordinates with one file for each day. 
The magnetic field magnitude and standard deviations of the vector components
are also included. 
 
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HEL2_6SEC_NESSMAG doi:10.48322/zxcr-jp63
Description
This dataset contains high resolution interplanetary magnetic field data in
six-second averages as measured by the Helios 1 tri-axial fluxgate magnetometer
experiment. Magnetic field vector components in nanotelsa [nT] are given in
solar-ecliptic (SE) spacecraft-centered coordinates with one file for each day. 
The magnetic field magnitude and standard deviations of the vector components
are also included. 
 
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HELIOS1_40SEC_MAG-PLASMA (spase://NASA/NumericalData/Helios1/E1/PT40.5S)
Description
General information about initial ascii files: This subdirectory contains daily
files of 40.5 sec Helios magnetic field and plasma data described below.  It
also contains a file of software written by Aaron Roberts,
readhelios40s_dat.pro, for creating alfvenicity graphs.       The Helios mission
consisted of two spacecraft launched into the inner heliosphere, both executing
orbits from 0.3 to 1 AU with roughly a six month orbital period.     Magnetic
field data were recorded at high resolution, with plasma data recorded  at
approximately 40.5 s resolution.  These datasets give the highest resolution 
plasma (proton and helium) moments with the corresponding average magnetic field
 for each plasma measurement.  There are results from two plasma sensors, one of
 which gives the vector velocity.         The coverage is best in the early
years and varies considerably for the rest of the mission.  The files
Helios1_stats and Helios2_stats give the year, day of  year, number of points,
and percentage of possible points for the days included  in the sets.  There is
no coverage for many days, with the main reason being that  the spacecraft pass
behind the Sun with respect to the Earth, thus cutting off  communication.      
       
The overall intervals covered are:  
Helios 1:  1974 day 346 to          
           1985 day 247              
Helios 2:  1976 day 017 to    
           1980 day 068       
The present set of files were produced by R. Schwenn and obtained from J.
Luhmann. They have been reformatted by Aaron Roberts to assure spaces between
the variables,  and in the process the HGI longitude and the RTN versions of the
variables were added for convenience.  Also, spacecraft positions were
interpolated to make them  distinct. The fill value for missing data in the
original files was either -1 or 0;  all these have been changed to 0. The other
entries are directly from the original  files.            
R. Schwenn should be acknowledged for plasma data and F. Neubauer for magnetic
field data.  GSFC/SPDF nssdcftp (or successor) should be acknowledged as the
immediate  source of the data.               
* The RTN components were calculated from the SSE XYZ components using R -> -X,
T -> -Y, and N -> Z.  The Cartesian coordinates for B and the angles for V are
the  original variables in the file, and no correction was made in the
conversion to RTN  for the actual spacecraft position.  Since RTN and SSE are
defined relative to the helioequatorial plane and to the ecliptic plane,
respectively, and since these planes are inclined by 7.25 degrees relative to
each other (heliocentric orbits of Earth,  Helios 1 and Helios 2 are virtually
co-planar), this introduces errors of up to 100% * (1 - cos 7.25) = 1% in the
RTN components.  However, the V and B are consistent with each other and can be
compared directly.                 
(text by Aaron Roberts, with edits by Joe King; October, 2008)  
 
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HELIOS1_COHO1HR_MERGED_MAG_PLASMA (spase://NASA/NumericalData/Helios1/MAGandPLS/PT1H)
Description
The HELIOS-1 spacecraft was one of the pair of deep space probes developed by
the Federal Republic of Germany (FRG) in a cooperative program with NASA.  The
purpose of the mission was to make pioneering measurements of the interplanetary
medium from the vicinity of the Earth's orbit to 0.3 AU. (The planet Mercury is
at 0.4 AU.)
Data coverage for selected parameters for this data set is: interplanetary 
magnetic  field (1974-12-14 - 1981-06-14), solar wind plasma (1974-12-12 -
1980-12-31), and spacecraft trajectory coordinates (1974-12-10 - 1981-06-14).
Magnetic field data were provided by Prof. F. Mariani, Istituto di Fisica G.
Marconi, Rome, Italy; Plasma data - by Dr. R. Schwenn, Max-Planck-Institut fur
Aeronomie, Lindau, Germany.
Time Coverage of merged files: December 10, 1974 - June 14, 1981.
Helios-1 data have been reprocessed to ensure a uniformity of content and
coordinate systems relative to data from other deep-space missions:
All spacecraft trajectory data were transformed to a Heliographic Inertial (HGI)
coordinate system.
Magnetic field components were transformed to RTN system.
Trajectory data, interplanetary magnetic field data, and plasma data were merged
into individual hourly records.
Data gaps were filled with dummy numbers for the missing hours or entire days to
make all files of equal length.  The character Ə' is used to fill all fields
for missing data according to their format, e.g. ' 9999.9' for a field with the
FORTRAN format F7.1. Note that format F7.1 below really means (1X,F6.1),etc.
 
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HELIOS1_E6_1HOUR_PARTICLE_FLUX (spase://NASA/NumericalData/Helios1/E6/ParticleFlux/PT1H)
Description
HELIOS-A and -B spacecrafts were the pair of deep space probes developed by the
Federal Republic of Germany (FRG) in a cooperative program with NASA. The
purpose of the mission was to make pioneering measurments of the interplanetary
medium from the vicinity of the earth"s orbit to 0.3 AU. 
The objective of experiment (E6) was to study high-energy, charged, cosmic-ray
particles of solar, planetary, and galactic origin in interplanetary space.
Protons and alpha particles with eneries >1.3 MeV/nucleon, and electrons >0.3
MeV were measured within interplanetary space over the range from 0.3 to 1.0 AU.
The instrument, a particle telescope with 55-deg field of view, consisted of
five semiconductor detectors, one sapphire Cherenkov counter, and one
scintillation counter, all enclosed by an anticoincidence cylinder. The
telescope was calibrated prior to launch using radioactive sources, particle
acceletors, and ground-level muons. It measured protons and alpha particles in
six channels (1.3-3.3, 3.3-13, 13-27, 27-37, 37-45, and >45 MeV/nucleon) and
electrons in five energy channels (0.3-0.8, 0.8-2, 2-3, 3-4, and >4 MeV). For
more detail see pp.253-257 of Raumfahrtforschung, v.19, n. 5, 1975. 
The h-a-cr*.dat and h-b-cr*.dat files contains hourly averaged fluxes of
electrons, protons and alpha particles in the MeV ranges. The files were written
in ASCII-codes. Each record contains 10 hourly averages. The differential fluxes
(particles/sq.m, s, sr, MeV) cover, in several bands, the energy range 0.3-2.0
MeV for electrons, 4.0-51 MeV for protons, and 2.0-48 MeV for alpha particles. 
Also provided are the integral fluxes of alphas above 48 MeV, and protons above
51 MeV. For some of the energy channels, the standard deviations of the averages
are also provided. Each file is preceded by a header record, providing the start
and stop times of the data in the file. 
The acronyms for the rate channels are composed of a letter and an indication of
the energy range in MeV/nucleon for protons and alpha particles respectively.
MeV for electrons. 
The counting rates are given as particles/m^2  sec sr MeV/N, except for the
integral channels P>51 and A>48 which are given as particles/ m^2 sec sr. 
Note: 1. Negative rates (-0.99999E+04) indicate missing or invalid data. 2. The
energy boundaries for the electron channels E 0.2-0.8 and E 0.8-2are only rough
estimates.
 
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HELIOS1_E6_KUNOW_1HOUR_PARTICLE-FLUX (spase://NASA/NumericalData/Helios1/E6/ParticleFlux/Kunow/CDF/PT1H)
Description
HELIOS-A and -B spacecrafts were the pair of deep space probes developed by the
Federal Republic of Germany (FRG) in a cooperative program with NASA. The
purpose of the mission was to make pioneering measurments of the interplanetary
medium from the vicinity of the earth"s orbit to 0.3 AU. 
The objective of experiment (E6) was to study high-energy, charged, cosmic-ray
particles of solar, planetary, and galactic origin in interplanetary space.
Protons and alpha particles with eneries >1.3 MeV/nucleon, and electrons >0.3
MeV were measured within interplanetary space over the range from 0.3 to 1.0 AU.
The instrument, a particle telescope with 55-deg field of view, consisted of
five semiconductor detectors, one sapphire Cherenkov counter, and one
scintillation counter, all enclosed by an anticoincidence cylinder. The
telescope was calibrated prior to launch using radioactive sources, particle
acceletors, and ground-level muons. It measured protons and alpha particles in
six channels (1.3-3.3, 3.3-13, 13-27, 27-37, 37-45, and >45 MeV/nucleon) and
electrons in five energy channels (0.3-0.8, 0.8-2, 2-3, 3-4, and >4 MeV). For
more detail see pp.253-257 of Raumfahrtforschung, v.19, n. 5, 1975. 
The h-a-cr*.dat and h-b-cr*.dat files contains hourly averaged fluxes of
electrons, protons and alpha particles in the MeV ranges. The files were written
in ASCII-codes. Each record contains 10 hourly averages. The differential fluxes
(particles/sq.m, s, sr, MeV) cover, in several bands, the energy range 0.3-2.0
MeV for electrons, 4.0-51 MeV for protons, and 2.0-48 MeV for alpha particles. 
Also provided are the integral fluxes of alphas above 48 MeV, and protons above
51 MeV. For some of the energy channels, the standard deviations of the averages
are also provided. Each file is preceded by a header record, providing the start
and stop times of the data in the file. 
The acronyms for the rate channels are composed of a letter and an indication of
the energy range in MeV/nucleon for protons and alpha particles respectively.
MeV for electrons. 
Note: 1. Negative rates (-0.99999E+04) indicate missing or invalid data. 2. The
energy boundaries for the electron channels E 0.2-0.8 and E 0.8-2are only rough
estimates.
 
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HELIOS1_HELIO1DAY_POSITION (spase://NASA/NumericalData/Helios1/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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HELIOS1_HELIO1HR_POSITION
Description
The hourly data are made by the linear interpolation of old daily files
 
Dataset in CDAWeb
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HELIOS2_40SEC_MAG-PLASMA (spase://NASA/NumericalData/Helios2/E3/PT40.5S)
Description
General information about initial ascii files: This subdirectory contains daily
files of 40.5 sec Helios magnetic field and plasma data described below.  It
also contains a file of software written by Aaron Roberts,
readhelios40s_dat.pro, for creating alfvenicity graphs.       The Helios mission
consisted of two spacecraft launched into the inner heliosphere, both executing
orbits from 0.3 to 1 AU with roughly a six month orbital period.     Magnetic
field data were recorded at high resolution, with plasma data recorded  at
approximately 40.5 s resolution.  These datasets give the highest resolution 
plasma (proton and helium) moments with the corresponding average magnetic field
 for each plasma measurement.  There are results from two plasma sensors, one of
 which gives the vector velocity.         The coverage is best in the early
years and varies considerably for the rest of the mission.  The files
Helios1_stats and Helios2_stats give the year, day of  year, number of points,
and percentage of possible points for the days included  in the sets.  There is
no coverage for many days, with the main reason being that  the spacecraft pass
behind the Sun with respect to the Earth, thus cutting off  communication.      
       
The overall intervals covered are:  
Helios 1:  1974 day 346 to          
           1985 day 247              
Helios 2:  1976 day 017 to    
           1980 day 068       
The present set of files were produced by R. Schwenn and obtained from J.
Luhmann. They have been reformatted by Aaron Roberts to assure spaces between
the variables,  and in the process the HGI longitude and the RTN versions of the
variables were added for convenience.  Also, spacecraft positions were
interpolated to make them  distinct. The fill value for missing data in the
original files was either -1 or 0;  all these have been changed to 0. The other
entries are directly from the original  files.            
R. Schwenn should be acknowledged for plasma data and F. Neubauer for magnetic
field data.  GSFC/SPDF nssdcftp (or successor) should be acknowledged as the
immediate  source of the data.               
* The RTN components were calculated from the SSE XYZ components using R -> -X,
T -> -Y, and N -> Z.  The Cartesian coordinates for B and the angles for V are
the  original variables in the file, and no correction was made in the
conversion to RTN  for the actual spacecraft position.  Since RTN and SSE are
defined relative to the helioequatorial plane and to the ecliptic plane,
respectively, and since these planes are inclined by 7.25 degrees relative to
each other (heliocentric orbits of Earth,  Helios 1 and Helios 2 are virtually
co-planar), this introduces errors of up to 100% * (1 - cos 7.25) = 1% in the
RTN components.  However, the V and B are consistent with each other and can be
compared directly.                 
(text by Aaron Roberts, with edits by Joe King; October, 2008)  
 
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HELIOS2_COHO1HR_MERGED_MAG_PLASMA (spase://NASA/NumericalData/Helios2/MAGandPLS/PT1H)
Description
The HELIOS-1 spacecraft was one of the pair of deep space probes developed by
the Federal Republic of Germany (FRG) in a cooperative program with NASA.  The
purpose of the mission was to make pioneering measurements of the interplanetary
medium from the vicinity of the Earth's orbit to 0.3 AU. (The planet Mercury is
at 0.4 AU.)
Data coverage for selected parameters for this data set is: interplanetary 
magnetic  field (1976-01-18 - 1980-03-04), solar wind plasma (1976-01-18 -
1980-03-04), and spacecraft trajectory coordinates (1976-01-18 - 1980-03-04).
Magnetic field data were provided by Prof. F. Mariani, Istituto di Fisica G.
Marconi, Rome, Italy; Plasma data - by Dr. R. Schwenn, Max-Planck-Institut fur
Aeronomie, Lindau, Germany.
Time Coverage of merged files: January 1, 1976 - March 4, 1980.
Helios-2 data have been reprocessed to ensure a uniformity of content and
coordinate systems relative to data from other deep-space missions:
All spacecraft trajectory data were transformed to a Heliographic Inertial (HGI)
coordinate system.
Magnetic field components were transformed to RTN system.
Trajectory data, interplanetary magnetic field data, and plasma data were merged
into individual hourly records.
Data gaps were filled with dummy numbers for the missing hours or entire days to
make all files of equal length.  The character Ə' is used to fill all fields
for missing data according to their format, e.g. ' 9999.9' for a field with the
FORTRAN format F7.1. Note that format F7.1 below really means (1X,F6.1),etc.
 
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HELIOS2_E6_1HOUR_PARTICLE_FLUX (spase://NASA/NumericalData/Helios2/E6/ParticleFlux/PT1H)
Description
HELIOS-A and -B spacecrafts were the pair of deep space probes developed by the
Federal Republic of Germany (FRG) in a cooperative program with NASA. The
purpose of the mission was to make pioneering measurments of the interplanetary
medium from the vicinity of the earth"s orbit to 0.3 AU. 
The objective of experiment (E6) was to study high-energy, charged, cosmic-ray
particles of solar, planetary, and galactic origin in interplanetary space.
Protons and alpha particles with eneries >1.3 MeV/nucleon, and electrons >0.3
MeV were measured within interplanetary space over the range from 0.3 to 1.0 AU.
The instrument, a particle telescope with 55-deg field of view, consisted of
five semiconductor detectors, one sapphire Cherenkov counter, and one
scintillation counter, all enclosed by an anticoincidence cylinder. The
telescope was calibrated prior to launch using radioactive sources, particle
acceletors, and ground-level muons. It measured protons and alpha particles in
six channels (1.3-3.3, 3.3-13, 13-27, 27-37, 37-45, and >45 MeV/nucleon) and
electrons in five energy channels (0.3-0.8, 0.8-2, 2-3, 3-4, and >4 MeV). For
more detail see pp.253-257 of Raumfahrtforschung, v.19, n. 5, 1975. 
The h-a-cr*.dat and h-b-cr*.dat files contains hourly averaged fluxes of
electrons, protons and alpha particles in the MeV ranges. The files were written
in ASCII-codes. Each record contains 10 hourly averages. The differential fluxes
(particles/sq.m, s, sr, MeV) cover, in several bands, the energy range 0.3-2.0
MeV for electrons, 4.0-51 MeV for protons, and 2.0-48 MeV for alpha particles. 
Also provided are the integral fluxes of alphas above 48 MeV, and protons above
51 MeV. For some of the energy channels, the standard deviations of the averages
are also provided. Each file is preceded by a header record, providing the start
and stop times of the data in the file. 
The acronyms for the rate channels are composed of a letter and an indication of
the energy range in MeV/nucleon for protons and alpha particles respectively.
MeV for electrons. 
The counting rates are given as particles/m^2  sec sr MeV/N, except for the
integral channels P>51 and A>48 which are given as particles/ m^2 sec sr. 
Note: 1. Negative rates (-0.99999E+04) indicate missing or invalid data. 2. The
energy boundaries for the electron channels E 0.2-0.8 and E 0.8-2are only rough
estimates.
 
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HELIOS2_E6_KUNOW_1HOUR_PARTICLE-FLUX (spase://NASA/NumericalData/Helios2/E6/ParticleFlux/Kunow/CDF/PT1H)
Description
HELIOS-A and -B spacecrafts were the pair of deep space probes developed by the
Federal Republic of Germany (FRG) in a cooperative program with NASA. The
purpose of the mission was to make pioneering measurments of the interplanetary
medium from the vicinity of the earth"s orbit to 0.3 AU. 
The objective of experiment (E6) was to study high-energy, charged, cosmic-ray
particles of solar, planetary, and galactic origin in interplanetary space.
Protons and alpha particles with eneries >1.3 MeV/nucleon, and electrons >0.3
MeV were measured within interplanetary space over the range from 0.3 to 1.0 AU.
The instrument, a particle telescope with 55-deg field of view, consisted of
five semiconductor detectors, one sapphire Cherenkov counter, and one
scintillation counter, all enclosed by an anticoincidence cylinder. The
telescope was calibrated prior to launch using radioactive sources, particle
acceletors, and ground-level muons. It measured protons and alpha particles in
six channels (1.3-3.3, 3.3-13, 13-27, 27-37, 37-45, and >45 MeV/nucleon) and
electrons in five energy channels (0.3-0.8, 0.8-2, 2-3, 3-4, and >4 MeV). For
more detail see pp.253-257 of Raumfahrtforschung, v.19, n. 5, 1975. 
The h-a-cr*.dat and h-b-cr*.dat files contains hourly averaged fluxes of
electrons, protons and alpha particles in the MeV ranges. The files were written
in ASCII-codes. Each record contains 10 hourly averages. The differential fluxes
(particles/sq.m, s, sr, MeV) cover, in several bands, the energy range 0.3-2.0
MeV for electrons, 4.0-51 MeV for protons, and 2.0-48 MeV for alpha particles. 
Also provided are the integral fluxes of alphas above 48 MeV, and protons above
51 MeV. For some of the energy channels, the standard deviations of the averages
are also provided. Each file is preceded by a header record, providing the start
and stop times of the data in the file. 
The acronyms for the rate channels are composed of a letter and an indication of
the energy range in MeV/nucleon for protons and alpha particles respectively.
MeV for electrons. 
Note: 1. Negative rates (-0.99999E+04) indicate missing or invalid data. 2. The
energy boundaries for the electron channels E 0.2-0.8 and E 0.8-2are only rough
estimates.
 
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HELIOS2_HELIO1DAY_POSITION (spase://NASA/NumericalData/Helios2/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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HELIOS2_HELIO1HR_POSITION
Description
The hourly data are made by the linear interpolation of old daily files
 
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HK_H0_MAG (spase://NASA/NumericalData/Hawkeye/MAG/PT1.9S)
Description
Gurnett, D. A., and L. A. Frank, A region of intense plasma wave turbulences on
auroral field lines, JGR, 82, 1031, 1977
Farrell, W. M., and J. A. Van Allen, Observations of the Earth"s  polar cleft at
large radial distances with Hawkeye 1 magnetometer, JGR, 95, 20945, 1990
Modification History
Created by S. Chen on 2-5-97
Modified by R. Kessel on 13 June 2000
 
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HK_H0_VLF doi:10.48322/etz7-wx98
Description
BUILD_DATE:                     1974-01-01
INSTRUMENT_MASS:         0.23 (LESS BOOMS) kg
INSTRUMENT_HEIGHT:       0.058 mt
INSTRUMENT_LENGTH:       0.140 mt
INSTRUMENT_WIDTH:         0.140 mt
INSTRUMENT_MANUFACTURER_NAME:   UNIV IOWA
INSTRUMENT_SERIAL_NUMBER:     VLF-05
                         Electric Antenna
The electric antenna on HAWKEYE consisted of two extendible beryllium copper
elements 0.025 inch in diameter which could be extended to a maximum tip-to-tip
length of 42.7 m. Except for the outermost 6.1 m of each element, which had a
conducting surface, the antenna was coated with Pyre-ML to electrically insulate
the antenna from the surrounding plasma. The insulating coating was required to
insulate the antenna from the perturbing effects of the plasma sheath
surrounding the spacecraft body. At high altitudes, the thickness of the plasma
sheath surrounding  the spacecraft body was quit large, on the order of 9 m.
Since the conducting portion of the antenna must extend beyond the plasma
sheath, it was necessary that the antenna be rather long, at least 30 m.
tip-to-tip. The antenna mechanism used on HAWKEYE was the Dual-Tee extendible
antenna manufactured by Fairchild Industries. The antenna length was 42.49
meters after final deployment until the last orbit, when an attempt was made to
retract the antenna to reduce the spacecraft drag.
                   Magnetic Antenna
 The magnetic antenna for this experiment consisted of a search coil with a high
permeability core mounted on a boom approximately 1.5 m. from the centerline of
the spacecraft body. The boom was a three element telescoping device developed
at the University of Iowa. The boom supporting the flux gate magnetometer on the
opposite side of the spacecraft was the same type. Both booms were extended
simultaneously by an electric motor.
           The search coil core was .305 m. long and was wound with
approximately 20,000 turns of copper wire. The axis of the search coil was
parallel to the spin axis of the spacecraft. A preamplifier was located with the
sensor to provide low-impedance signals to the main electronics package in the
spacecraft body. The frequency range of the search coil antenna was from 1.0 Hz
to 10.0 kHz.
                         Electronics
 The potential difference between the electric antenna elements was amplified by
a high input impedance differential amplifier to provide a 0 to 5 volt analog
voltage, V-Diff, to the spacecraft encoder. As the spacecraft rotated the
potential difference between the antenna elements  varied sinusoidally at the
spacecraft rotation rate, with an amplitude proportional to the electric field
strength and a phase determined by the direction of the electric field. The
frequency response of the differential amplifier was 0.05 Hz to 10 Hz and
included the entire range of spin rates expected as the antenna was deployed.
The V-Diff signal was sampled 6 times each frame by the encoder. The gain of the
differential amplifier could be controlled by command to provide dynamic ranges
of +/-0.5 and +/-8.0 volts for the antenna potential difference measurements.
           Signals from the electric antenna in the frequency range from 10 kHz
to 200 kHz were analyzed by the narrow band step frequency receiver. The primary
purpose of this receiver was to provide very good frequency resolution in the
neighborhood of the electron plasma frequency and upper hybrid resonance
frequency. The step frequency receiver consisted of 8 narrow band filters (+/-5%
band-width) which were sequentially switched into a log compressor. The  log
compressor provided a 0 to 5 volt analog voltage, SFR, to the spacecraft
encoder. The switch (S4) position was controlled by clock lines from the
spacecraft encoder and was stepped through 8 frequencies, 13.3, 17.8, 23.7,
31.1, 42.2, 56.2, 100, and 178 kHz, at a rate of four frequencies per telemetry
frame (5.76 seconds). The log compressor provided a 0 to 5 volt analog voltage,
SFR, to the spacecraft encoder which was proportional to the logarithm of the
signal strength over a dynamic range of 100 db.
           The 8-channel spectrum analyzer  provided relatively coarse frequency
spectrum measurements of both electric and magnetic fields over a broad
frequency range of 1.0 Hz to 10.0 kHz. The primary purpose of the 8-channel
spectrum analyzer was to provide field strength measurements to complement the
high-resolution frequency-time spectra from the wide-band receiver.
           Switches S1 and S2 were controlled by clock lines from the spacecraft
encoder and commutate the filter outputs to two log compressors which provided
field strength measurements SA-1 and SA-2 (0 to 5 volts) to the spacecraft
encoder. These outputs were sampled twice per telemetry frame. Switch S3, which
was controlled by a clock line, commutates the electric and magnetic field
signals to the 8-channel spectrum analyzer.
          Approximately every 5 minutes the impedance of the electric antenna
was determined at a frequency of 17 Hz by driving a small AC current into the
antennas and measuring the resultant voltage on the antennas with the 8-channel
spectrum analyzer. The 17 Hz oscillator was gated on for 1 frame out of every 64
frames by a clock line.
           Immediately following the impedance measurement the pulser circuit
produced a 10 volt pulse with a duration of 20 micro- seconds. This pulse was to
stimulate local plasma resonances, such as plasma oscillation, from which the
electron density could be determined. A pulse of +10 volts was applied to one
antenna element and a -10 volt pulse was applied to the opposite antenna
element. The pulser was switched on by command. The pulser was on when the
experiment was in VLF45 mode and off when the experiment was in the VLF10 mode.
The pulser voltage was coupled to the antenna through a 220 pf capacitor which
would have allowed some meaningful data to be obtained from the experiment even
if the pulser output were to short to ground. The pulse was applied at the end
of the impedance measurement frame.
 The potential difference between the electric antenna elements was amplified by
a high input impedance differential amplifier to provide a 0 to 5 volt analog
voltage, V-Diff, to the spacecraft encoder. As the spacecraft rotated the
potential difference between the antenna elements  varied sinusoidally at the
spacecraft rotation rate, with an amplitude proportional to the electric field
strength and a phase determined by the direction of the electric field. The
frequency response of the differential amplifier was 0.05 Hz to 10 Hz and
included the entire range of spin rates expected as the antenna was deployed.
The V-Diff signal was sampled 6 times each frame by the encoder. The gain of the
differential amplifier could be controlled by command to provide dynamic ranges
of +/-0.5 and +/-8.0 volts for the antenna potential difference measurements.
           Signals from the electric antenna in the frequency range from 10 kHz
to 200 kHz were analyzed by the narrow band step frequency receiver. The primary
purpose of this receiver was to provide very good frequency resolution in the
neighborhood of the electron plasma frequency and upper hybrid resonance
frequency. The step frequency receiver consisted of 8 narrow band filters (+/-5%
band-width) which were sequentially switched into a log compressor. The  log
compressor provided a 0 to 5 volt analog voltage, SFR, to the spacecraft
encoder. The switch (S4) position was controlled by clock lines from the
spacecraft encoder and was stepped through 8 frequencies, 13.3, 17.8, 23.7,
31.1, 42.2, 56.2, 100, and 178 kHz, at a rate of four frequencies per telemetry
frame (5.76 seconds). The log compressor provided a 0 to 5 volt analog voltage,
SFR, to the spacecraft encoder which was proportional to the logarithm of the
signal strength over a dynamic range of 100 db.
           The 8-channel spectrum analyzer  provided relatively coarse frequency
spectrum measurements of both electric and magnetic fields over a broad
frequency range of 1.0 Hz to 10.0 kHz. The primary purpose of the 8-channel
spectrum analyzer was to provide field strength measurements to complement the
high-resolution frequency-time spectra from the wide-band receiver.
           Switches S1 and S2 were controlled by clock lines from the spacecraft
encoder and commutate the filter outputs to two log compressors which provided
field strength measurements SA-1 and SA-2 (0 to 5 volts) to the spacecraft
encoder. These outputs were sampled twice per telemetry frame. Switch S3, which
was controlled by a clock line, commutates the electric and magnetic field
signals to the 8-channel spectrum analyzer.
          Approximately every 5 minutes the impedance of the electric antenna
was determined at a frequency of 17 Hz by driving a small AC current into the
antennas and measuring the resultant voltage on the antennas with the 8-channel
spectrum analyzer. The 17 Hz oscillator was gated on for 1 frame out of every 64
frames by a clock line.
           Immediately following the impedance measurement the pulser circuit
produced a 10 volt pulse with a duration of 20 micro- seconds. This pulse was to
stimulate local plasma resonances, such as plasma oscillation, from which the
electron density could be determined. A pulse of +10 volts was applied to one
antenna element and a -10 volt pulse was applied to the opposite antenna
element. The pulser was switched on by command. The pulser was on when the
experiment was in VLF45 mode and off when the experiment was in the VLF10 mode.
The pulser voltage was coupled to the antenna through a 220 pf capacitor which
would have allowed some meaningful data to be obtained from the experiment even
if the pulser output were to short to ground. The pulse was applied at the end
of the impedance measurement frame.
Modification History
CDF created Jan 1999 by Mona Kessel
modified Aug 1999 by Mona Kessel, Carolyn Ng
modified Oct 1999 by Mona Kessel
modified Nov 1999 by Mona Kessel, final for archiving
 
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HYAKUTAKE_HELIO1DAY_POSITION (spase://NASA/NumericalData/Comet/Hyakutake/HelioWeb/Ephemeris/P1D)
Description
No TEXT global attribute value.
 
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HYAKUTAKE_HELIO1HR_POSITION
Description
No TEXT global attribute value.
 
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I1_AV2_OTT (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Version2/Ottawa/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 673). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://spdf.gsfc.nasa.gov/isis/isis-status.html 
Modification History
created December 2017
 
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I1_AV2_QUI (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Version2/Quito/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 673). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://spdf.gsfc.nasa.gov/isis/isis-status.html 
Modification History
created December 2017
 
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I1_AV2_SNT
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 673). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://spdf.gsfc.nasa.gov/isis/isis-status.html 
Modification History
created December 2017
 
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I1_AV2_ULA (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Version2/Fairbanks/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 673). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://spdf.gsfc.nasa.gov/isis/isis-status.html 
Modification History
created December 2017
 
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I1_AV_ALL (spase://NASA/NumericalData/ISIS1/SFS/Ionogram/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_KER (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/KerguelenIsland/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_KSH (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Kashima/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_KWA (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Kwajalein/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_ODG (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Ouagadougou/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_ORR (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Orroral/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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I1_AV_OTT (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Ottawa/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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Data Access Code Examples written in Python and IDL®.
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I1_AV_QUI (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Quito/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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Data Access Code Examples written in Python and IDL®.
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I1_AV_RES (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/ResoluteBay/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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Data Access Code Examples written in Python and IDL®.
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I1_AV_SNT (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Santiago/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I1_AV_SOD (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Sodankyla/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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Data Access Code Examples written in Python and IDL®.
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I1_AV_TRO (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Tromso/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I1_AV_ULA (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Fairbanks/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I1_AV_WNK (spase://NASA/NumericalData/ISIS1/SFS/AverageIonogram/Winkfield/PT29S)
Description
This ionogram was digitized from the original ISIS 1 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1998
 
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Data Access Code Examples written in Python and IDL®.
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I1_NEPROF_TOPS (spase://NASA/NumericalData/ISIS1/SFS/TOPS)
Description
This data set, provided by the Communications Research Centre (CRC) in Ottawa,
Canada, consists of electron density profiles for the ionosphere above the F2
maximum (topside ionosphere). The data were computed from the orginal ionograms
using Jackson's method (Jackson, Proceedings of the IEEE., p. 960, June 1969).
ISIS-1 was launched on 1969-01-30 into an elliptical orbit (500-3500km) with an
inclination of 88.4 degrees and ISIS-2 was launched on 1971-04-01 into an
circular orbit at 1400 km with an inclination of 88.1 degrees.
Both satellites were fully instrumented ionospheric observatories including
sweep- and fixed-frequequency ionosondes, a VLF receiver, energetic and soft
particle detectors, an ion mass spectrometer, an electrostatic analyzer, an
Langmuir probe, a beacon transmitter, a cosmic noise experiment and ISIS 2 also
carried two photometers. A tape recorder with 1-h capacity was included on both
satellites. Data were also collected during overflights of several telemetry
stations. The telemetry stations were in areas that provided primary data
coverage near the 80-deg-W meridian and in areas near Hawaii, Singapore,
Australia, the UK, Norway, India, Japan, Antarctica, New Zealand, and Central
Africa.
 
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I2_AV_ACN (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/AscensionIsland/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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Data Access Code Examples written in Python and IDL®.
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I2_AV_ADL (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/TerreAdelie/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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Data Access Code Examples written in Python and IDL®.
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I2_AV_AME (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Ahmedabad/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_BRZ (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Brazzaville/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_BUR (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Johannesburg/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_CNA (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/LasPalmas/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_KER (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/KerguelenIsland/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_KRU (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Kourou/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_KSH (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Kashima/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_KWA (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Kwajalein/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_LAU (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Lauder/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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I2_AV_ODG (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Ouagadougou/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
Dataset in CDAWeb
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I2_AV_ORR (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Orroral/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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I2_AV_OTT (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Ottawa/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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I2_AV_QUI (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Quito/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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I2_AV_RES (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/ResoluteBay/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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I2_AV_SNT (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Santiago/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_AV_SOD (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Sodankyla/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_AV_SOL (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/FalklandIslands/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_AV_SYO (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/SyowaBase/PT22S)
Description
A 7-track ISIS 2 analog telemetry tape from Ottawa (#561) has been 
digitized using the GSFC facilities of the Data Evaluation Laboratory 
(DEL) within the Mission Operations and Data Systems Directorate (Code 
500) at Goddard.  The digitization was performed using an A/D 
converter board and software device driver compatible with the OS/2 
operating system used by the 486-based Programmable Telemetry 
Processor (PTP) associated software has been installed on their PTP 
and de-bugged so that we now have a working system for making digital 
ISIS ionograms directly from the telemetry tapes.  Earlier, we 
successfully digitized the PCM and NASA 36 bit time-code data from 
this same tape. The ionograms were digitized at the rate of 40,000 
16-bit samples/sec. This sample rate is higher than the Nyquist 
frequency of 30 kHz appropriate for the post-detection ISIS 2 
sounder-receiver video output which extends from DC to 15 kHz (see p. 
50 of the 1971 ISIS 2 report by Daniels).  The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (ct/2) interval of 3.747 km.  With the ISIS 2 prf of 45 
sounder pulses/s, there are (1/45)/(2.5**(-5)) = 888.89 samples 
between each of the approximately 1015 sounder pulses per ionogram 
(including the fixed-frequency portion) or nearly 10**6 16-bit 
samples/ionogram (approximately 1.8 MBytes) for just the 
sounder-receiver video data. Adding header information, and the pcm 
data containing data from the other instruments, yields about 2 MBytes 
of data for the 22.5 s period corresponding to one ionogram. Two steps 
were taken in order to reduce this large volume of nearly 2 
MBytes/ionogram.  First, every four 25 microsecond samples following 
the sounder pulse were averaged.  Second, the 16 bit samples were 
reduced to 8 bit samples.  The first step decreased the apparent-range 
resolution to 15 km, but yielded high-quality ionograms because of the 
improved S/N due to the averaging. 
Modification History
created April 1995
 
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I2_AV_TRO (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Tromso/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_AV_ULA (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Fairbanks/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_AV_WNK (spase://NASA/NumericalData/ISIS2/SFS/AverageIonogram/Winkfield/PT22S)
Description
This ionogram was digitized from the original ISIS 2 analog 
telemetry data on 7-track tape using the facilities of the Data 
Evaluation Laboratory at GSFC (Code 500). This data restoration 
project is headed by Dr. R.F. Benson (GSFC, Code 692). Ionograms were 
digitized at the rate of 40,000 16-bit samples/sec. This sample rate is 
higher than the Nyquist frequency of 30 kHz. The sample frequency of 40 
kHz provides a measurement every 25 microseconds corresponding to an 
apparent range (c*t/2) interval of 3.747 km. Each ionogram consists 
of a fixed-frequency and and a swept-frequency portion. The time 
resolution is typically 24 seconds. More information can be found 
at https://nssdc/space/isis/isis-status.html 
Modification History
created April 1995
 
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I2_NEPROF_TOPIST (spase://NASA/NumericalData/ISIS2/SFS/TOPIST)
Description
ISIS 2 was an ionospheric observatory instrumented with a sweep- and a
fixed-frequency ionosonde, a VLF receiver, energetic and soft particle
detectors, an ion mass spectrometer, an electrostatic probe, a retarding
potential analyzer, a beacon transmitter, a cosmic noise experiment, and two
photometers. Two long crossed-dipole antennas (73 and 18.7 m) were used for the
sounding, VLF, and cosmic noise experiments.
The spacecraft was spin-stabilized to about 2 rpm after antenna deployment.
There were two basic orientation modes for the spacecraft, cartwheel and
orbit-aligned. The spacecraft operated approximately the same length of time in
each mode, remaining in one mode typically 3 to 5 months. The cartwheel mode
with the axis perpendicular to the orbit plane was made available to provide ram
and wake data for some experiments for each spin period, rather than for each
orbit period. Attitude and spin information was obtained from a three-axis
magnetometer and a sun sensor. Control of attitude and spin was possible by
means of magnetic torquing.
The experiment package also included a programmable tape recorder with a one
hour capacity. For non-recorded observations, data from satellite and
subsatellite regions were telemetered when the spacecraft was in the line of
sight of a telemetry station. Telemetry stations were located so that primary
data coverage was near the 80-deg-W meridian and near Hawaii, Singapore,
Australia, England, France, Norway, India, Japan, Antarctica, New Zealand, and
Central Africa. NASA support of the ISIS project was terminated on October 1,
1979.  
A significant amount of experimental data, however, was acquired after this date
by the Canadian project team. ISIS 2 operations were terminated in Canada on
March 9, 1984. The Radio Research Laboratories (Tokyo, Japan) then requested and
received permission to reactivate ISIS 2. Regular ISIS 2 operations were started
from Kashima, Japan, in early August 1984. ISIS 2 was deactivated effective 24,
1990. A data restoration effort began in the late 1990s and successfully saved a
considerable portion of the high-resolution data before the telemetry tapes were
discarted.
The data set was generated from the averaged ionogram binary data (SPIO-00318)
recorded by the Topside Sounder. The data are obtained with the TOPIST program,
which analyzes the data, automatically scales the ionogram traces and
resonances, and inverts the traces into an electron density profile. The same
program is available for use to hand-scale the data if desired. Output data
items include spacecraft position, electron density profile, assessment of
quality, resonance and cut-off frequencies, and both the O-trace and X-trace.
 
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I2_NEPROF_TOPS (spase://NASA/NumericalData/ISIS2/SFS/TOPS)
Description
This data set, provided by the Communications Research Centre (CRC) in Ottawa,
Canada, consists of electron density profiles for the ionosphere above the F2
maximum (topside ionosphere). The data were computed from the orginal ionograms
using Jackson's method (Jackson, Proceedings of the IEEE., p. 960, June 1969).
ISIS-1 was launched on 1969-01-30 into an elliptical orbit (500-3500km) with an
inclination of 88.4 degrees and ISIS-2 was launched on 1971-04-01 into an
circular orbit at 1400 km with an inclination of 88.1 degrees.
Both satellites were fully instrumented ionospheric observatories including
sweep- and fixed-frequequency ionosondes, a VLF receiver, energetic and soft
particle detectors, an ion mass spectrometer, an electrostatic analyzer, an
Langmuir probe, a beacon transmitter, a cosmic noise experiment and ISIS 2 also
carried two photometers. A tape recorder with 1-h capacity was included on both
satellites. Data were also collected during overflights of several telemetry
stations. The telemetry stations were in areas that provided primary data
coverage near the 80-deg-W meridian and in areas near Hawaii, Singapore,
Australia, the UK, Norway, India, Japan, Antarctica, New Zealand, and Central
Africa.
 
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I7_R0_LEPEDEA
Description
No TEXT global attribute value.
 
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I8_15SEC_MAG doi:10.48322/pxb6-h511
Description
This 15.36s data set was created in 2008-9 at GSFC/SPDF from a newly created
320ms data set, with some gaps filled with data from the prior 15.36s data set.
Full documentation may be found at
https://spdf.gsfc.nasa.gov/pub/data/imp/imp8/mag/15s_ascii_v3/00_IMP8_15s_data_d
ocum.txt Creation of the new 320ms and 15.36s data sets was done by N.
Papitashvili and J. King, with guidance from Adam Szabo. 
Modification History
Master CDF made 02/16/10 by N. E. Papitashvili, SPDF Modified to revised form
v03 on 02/16/10.
 
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I8_320MSEC_MAG doi:10.48322/k2cv-vy73
Description
For detailed documentation on the creation of this data set see 
https://spdf.gsfc.nasa.gov/pub/data/imp/imp8/mag/320ms_ascii/doc/imp8_mag_320ms_
proc.txt
 
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I8_H0_GME doi:10.48322/m36p-0998
Description
30-min avg flex I8 GME
Modification History
v0.1 (vv01) May/Aug97  orig 30-min design V0.2 (vv02) Nov97  split protons into 
two vars by energies  (not needed virvars) V0.3 (vv03) Jul/Aug98  cleaned up var
names & set up for virvars V0.4 (vv04) Aug98  defined virvars for  alternate
views
 
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I8_H0_MITPLASMA doi:10.48322/4dhv-w146
Description
See online MIT documentation
Modification History
 CDF versions created August 2004
 
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I8_OR_GIFWALK
Description
Pre-generated ISTP orbit plots
 
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I8_OR_SSC (spase://NASA/NumericalData/IMP8/Ephemeris/PT12M)
Description
Generated by SSCWeb from Heather Franz's "Second Experimental Ephemeris" as
approved by IMP-8 PIs 
Modification History
Originated 03/14/96
 
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I8_R0_LEPEDEA
Description
No TEXT global attribute value.
 
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IA_K0_ENF (spase://NASA/NumericalData/Interball-2/SK3/KP/PT120S)
Description
Measurements of spectra and anisotropy of electrons witin energy ranges 20-40
keV from two time-of-flight detectors EM-1-1 and EM-1-2. The field of view of
these detectors are directed oppositely and perpendicular to the satellite 
rotation axis. 
Data description:  http://www.iki.rssi.ru/inte rball.html  
Modification History
created Sep 1998
 
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IA_K0_EPI (spase://NASA/NumericalData/Interball-2/DOK2A/KP/PT120S)
Description
No TEXT global attribute value.
Modification History
created Apr 1997
 
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IA_K0_ICD (spase://NASA/NumericalData/Interball-2/PROMICS3/KP/PT120S)
Description
Count rate of H+, O+ ions in 2 min, three directions, (1-30 keV) Status flag
shows instrument mode.
Data description:  http://www.iki.rssi.ru/interball.html 
Modification History
created Sep 1998
 
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IA_K0_MFI (spase://NASA/NumericalData/Interball-2/IMAP3/PT120S)
Description
Full description: http://www.iki.rssi.ru/interball.html 
Full description: http://www.iki.rssi.ru/interball.html 
Modification History
created May 1997
 
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IA_OR_DEF (spase://NASA/NumericalData/Interball-2/Ephemeris/PT120S)
Description
Full description: http://www.iki.rssi.ru/interball.html 
Full description: http://www.iki.rssi.ru/interball.html 
Modification History
created May 1997
edited global attributes Apr 1996
 
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IBEX_H3_ENA_HI_R02_CG_NOSP_OMNI_6MO doi:10.48322/rcw2-kh18
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 17
releases of IBEX-HI and/or IBEX-LO data covering 2009-2020. 
2: This data set is from the Release 2 (6 months-cadence) IBEX-Hi map data for
the year 2009 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 2 map numbers (1-2) with mission year 1
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
8: This particular data set, denoted in the original ascii files as mapN for
N=1-2, which indicates a map number, includes pixel map data from all directions
(omnidirectional), CG, no SP, 6 month cadence. 
 
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IBEX_H3_ENA_HI_R02_NOCG_NOSP_OMNI_6MO doi:10.48322/0vjh-ph32
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 17
releases of IBEX-HI and/or IBEX-LO data covering 2009-2020. 
2: This data set is from the Release 2 (6 months-cadence) IBEX-Hi map data for
the year 2009 in the form of omnidirectional ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 2 map numbers (1-2) with mission year 1
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
8: This particular data set, denoted in the original ascii files as mapN for
N=1-2, which indicates a map number, includes pixel map data from all directions
(omnidirectional), no CG, no SP, 6 month cadence. 
 
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IBEX_H3_ENA_HI_R04_CG_NOSP_ANTIRAM_1YR doi:10.48322/8m6t-z779
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_yearN_cg for N  1 - 3, includes pixel map data from antiram
direction (antiram-directional), CG, no SP, 1 year cadence. 
Modification History
Currently, the Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_CG_NOSP_OMNI_6MO doi:10.48322/bfkf-5y54
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (6 months-cadence) IBEX-Hi map data for
the years 2009-2012 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction (nosp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_mapX for N=1-6, in which N indicates a map number, includes pixel map
data from all directions (omnidirectional), CG, no SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_CG_NOSP_RAM_1YR doi:10.48322/4ey3-fd10
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_yearN_cg  for N = 1 - 3, includes pixel map data from ram
direction (ram-directional), CG, no SP, 1 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_CG_SP_ANTIRAM_1YR doi:10.48322/db3x-tq55
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_yearN_cg for N = 1 - 3, includes pixel map data from
antiram direction (antiram-directional), CG, SP, 1 year cadence. 
Modification History
Currently, the Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R04_CG_SP_OMNI_6MO doi:10.48322/c9gv-sz19
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (6 months-cadence) IBEX-Hi map data for
the years 2009-2012 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_mapN for N = 1 - 6, in which N indicates a map number, includes
pixel map data from all directions (omnidirectional), CG, SP, 6 month cadence. 
Modification History
The newest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_CG_SP_RAM_1YR doi:10.48322/55hv-vx14
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_yearN_cg for N = 1 - 3, includes pixel map data from ram
direction (ram-directional), CG, SP, 1 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_DEFLECTION_1AU_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.defl1au , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R04_DEFLECTION_SCF_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.deflscf , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R04_LOSS_1AU_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.loss1au , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R04_LOSS_SCF_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.lossscf , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R04_NOCG_NOSP_ANTIRAM_1YR doi:10.48322/c3kb-p352
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of antiram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_yearN for N = 1 - 3, includes pixel map data from antiram
direction (antiram-directional), no CG, no SP, 1 year cadence. 
Modification History
Currently, the Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_3YR doi:10.48322/qmwe-ve75
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2011. 
2: This data set is from the Release 4 three-year IBEX-Hi map data for
2009-2011, in the form of omni-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) and with no corrections (nosp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 4 map numbers (1-6) with mission year
(1-3) each year is associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
8: This particular data set, denoted in the original ascii files as
comb-year123, includes pixel map data from omni direction, noCG, noSP, 3 year
cadence. 
Modification History
The Release 4 data extend through Map 6 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_6MO doi:10.48322/kef0-gf62
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (6 months-cadence) IBEX-Hi map data for
the  years 2009-2012 in the form of omnidirectional ENA (hydrogen) fluxes with
no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
no correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as hvset_mapN
for N=1-6, which indicates a map number, includes pixel map data from all
directions (omnidirectional), no CG, no SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_NOSP_OMNI_6MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2011. 
2: This data set is from the Release 4 three-year IBEX-Hi map data for
2009-2011, in the form of omni-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) and with no corrections (nosp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.)
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 4 map numbers (1-6) with mission year
(1-3) each year is associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
8: This particular data set, denoted in the original ascii files as
comb-map1to6, includes pixel map data from omni direction, noCG, noSP, 6 maps or
3 year cadence. 
Modification History
The Release 4 data extend through Map 6 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_NOSP_RAM_1YR doi:10.48322/v4rn-nd04
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of ram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_N for N = 1 - 3, includes pixel map data from ram direction
(ram-directional), no CG, no SP, 1 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_SP_ANTIRAM_1YR doi:10.48322/wgdc-pg68
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2012 in the form of antiram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
withcorrection for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_yearN for N = 1 - 3, includes pixel map data from antiram
direction (antiram-directional), no CG, SP, 1 year cadence. 
Modification History
The Release 4 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_SP_OMNI_6MO doi:10.48322/wvkh-8a67
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 6 (6 months-cadence) IBEX-Hi map data for
the years 2009-2012 in the form of omnidirectional ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_mapN for N=1 - 6, which indicates a map number, includes pixel map
data from all directions (omnidirectional), no CG, SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_NOCG_SP_RAM_1YR doi:10.48322/yf48-sn54
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4 (1 year-cadence) IBEX-Hi map data for the
years 2009-2019 in the form of ram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
withcorrection for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_yearN for N = 1 - 3, includes pixel map data from ram
direction (ram-directional), no CG, SP, 1 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_SURVPRO_1AU_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.survscf , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R04_SURVPRO_SCF_7DAY
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 4, 7.5 day-cadence IBEX-Hi data for the 
years 2009-2012 in the form of Survival Probabilities tables. Each data
directory related to survival probability has information about a different
aspect of the transport through the heliosphere: 
a) deflection - angular deflection experienced between the termination shock and
the observer. 
b) eloss - energy loss (or gain) between the termination shock and the observer.
c) survpro - survival probability that an ENA passing through the termination
shock will make it to 1AU. 
3. For this release, the survival probabilities are only applied to the IBEX-HI
data stream. Note that the energy loss is negligible, and the deflection angles
in the inertial system are always smaller than 0.6 degrees or so. 
4. Each directory has contains correction factors for data in the spacecraft
frame (scf) and the inertial frame (1AU). The inertial frame (1AU) survival
probabilities are used for the CG corrected data. The spacecraft frame factors
are used for uncorrected data. The spacecraft frame files have the
energy/direction shifts caused by the Earth/Spacecraft motion. This has a small
effect on the survival probabilities (simply due to the energy shifts), but the
deflection angles and energy shifts caused by this motion can be significant. 
5. The deflection and energy shift files are not applied by the IBEX pipeline
software. In theory, these could be applied to the CG corrected data after the
fact. However, it is important to note that the spacecraft frame correction
factors for energy and angle contain elements of the CG correction and 
6. can yield confusing results when applied to the pipeline results. The data
layout per frame consists of the following. For the spacecraft frame, there is a
column for each ESA step, and a row for each angle bin (1 degree bins). Each
number gives the probability at that angle and ESA for survival. The probability
per angle is interpolated to the center of any particular angular bin being
evaluated. In the inertial frame, the columns are the energies rather than ESA
steps. 
7. These are applied to the IBEX images that are given on the variable energy
grid. For each image pixel, we take the energy and angle and use a 2D
interpolation to get the survival probability.
8. The data consist of Survival Probabilities tables. Details of the data and
enabled science from Release 10 are given in the following journal publication:
9: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
10: http://doi.org/10.3847/1538-4365/aa66d8  
8: This particular data set, denoted in the original ascii files as
Data_Release_4\hs_transport\surv\o0NNNx.survscf , where NNN=006-150 is an orbit
number, and x = a or b for the orbit 130 or higher, indicates the first or the
second half of the orbit, Survival Probabilities tables
Modification History
The latest Release 16 data extends through Map 22 and contains modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_CG_NOSP_ANTIRAM_MIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Mono Inertial Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_year_1to5combinedMonoInertialFrame are pixel map data
antiram-directional in Mono Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_CG_NOSP_ANTIRAM_VEIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_year_1to5combinedVarEnergyInertialFrame are pixel map data
antiram-directional in Var Energy Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_6MO doi:10.48322/2hfb-zn61
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction (nosp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_mapX, where X = 1-10 are pixel map data from all directions
(omnidirectional), CG, no SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_MIF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Mono Inertial Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_map_1to10combinedMonoInertialFrame are pixel map data from all
directions (omnidirectional) in Mono Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_NOSP_OMNI_VEIF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_map_1to10combinedVarEnergyInertialFrame are pixel map data from all
directions (omnidirectional) in Var Energy Inertial Frame, CG, no SP, 5 year
cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_1YR doi:10.48322/aper-3h74
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_yearN for N=1,5, includes pixel map data from ram direction
(ram-directional), CG, no SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_MIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Mono Inertial Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SCF Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_year_1to5combinedMonoInertialFrame are pixel map data
ram-directional in Mono Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_NOSP_RAM_VEIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
no correction (nosp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_year_1to5combinedVarEnergyInertialFrame are pixel map data
ram-directional in Var Energy Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_1YR doi:10.48322/q5mq-2v40
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_yearN for N=1,5, includes pixel map data from antiram
direction (antiram-directional), CG, SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_MIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Mono Inertial Frame between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SCF Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_year_1to5combinedMonoInertialFrame are pixel map data
antiram-directional in Mono Inertial Frame, CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_SP_ANTIRAM_VEIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_year_1to5combinedVarEnergyInertialFrame are pixel map
data antiram-directional in Var Energy Inertial Frame, CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R07_CG_SP_OMNI_6MO doi:10.48322/dz2p-nd24
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (6 months-cadence) IBEX-Hi map data for
the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_mapX, where X = 1-10 are pixel map data from all directions
(omnidirectional), CG, SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_CG_SP_OMNI_MIF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Mono Inertial Frame between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_map_1to10combinedMonoInertialFrame are pixel map data from all
directions (omnidirectional) in Mono Inertial Frame, CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_SP_OMNI_VEIF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_map_1to10combinedVarEnergyInertialFrame are pixel map data from all
directions (omnidirectional) in Var Energy Inertial Frame, CG, SP, 5 year
cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_CG_SP_RAM_1YR doi:10.48322/qmwd-ct89
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_yearN for N=1,5, includes pixel map data from ram direction
(ram-directional), CG, SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_CG_SP_RAM_MIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Mono Inertial Frame between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_year_1to5combinedMonoInertialFrame are pixel map data
ram-directional in Mono Inertial Frame, CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R07_CG_SP_RAM_VEIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability in Var Energy Inertial Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_year_1to5combinedVarEnergyInertialFrame are pixel map data
ram-directional in Var Energy Inertial Frame, CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_ANTIRAM_1YR doi:10.48322/ytmb-dg43
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of antiram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_yearN for N=1,5, includes pixel map data from antiram
direction (antiram-directional), no CG, no SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_ANTIRAM_VESCF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and no correction (nosp) for ENA survival probability in Var Energy SC Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_year_1to5combinedVarEnergySCFrame are pixel map data
antiram-directional in Var Energy SC Frame, no CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_OMNI_6MO doi:10.48322/33ew-ce35
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction (nosp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as hvset_mapX,
where X = 1-10 are pixel map data from all directions (omnidirectional), no CG,
no SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_OMNI_VESCF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with noCompton-Getting correction (nocg) of flux spectra for spacecraft  motion
and no correction (nosp) for ENA survival probability in Var Energy SC Frame
between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_map_1to10combinedVarEnergySCFrame are pixel map data from all directions
(omnidirectional) in Var Energy SC Frame, no CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_RAM_1YR doi:10.48322/p855-9622
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of ram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_yearN for N=1,5, includes pixel map data from ram direction
(ram-directional), no CG, no SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_NOCG_NOSP_RAM_VEIF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and no correction (nosp) for ENA survival probability in Var Energy Inertial
Frame between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_year_1to5combinedVarEnergyInertialFrame are pixel map data
ram-directional in Var Energy Inertial Frame, no CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_NOCG_SP_ANTIRAM_1YR doi:10.48322/ak3m-pg10
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of antiram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_SP_antiram_nocg_yearN for N=1,5, includes pixel map data from antiram
direction (antiram-directional), no CG, SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_NOCG_SP_ANTIRAM_VESCF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of antiram-directional ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and correction (sp) for ENA survival probability in Var Energy SC Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_year_1to5combinedVarEnergySCFrame are pixel map data
antiram-directional in Var Energy SC Frame, no CG, no SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R07_NOCG_SP_OMNI_6MO doi:10.48322/16jb-2837
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft motion and
correction (sp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_mapX, where X = 1-10 are pixel map data from all directions
(omnidirectional), no CG, SP, 6 month cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R07_NOCG_SP_OMNI_VESCF_10MP
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-10-map-average) IBEX-Hi map data
for the years 2009-2014 in the form of omnidirectional ENA (hydrogen) fluxes
with noCompton-Getting correction (nocg) of flux spectra for spacecraft  motion
and correction (sp) for ENA survival probability in Var Energy SC Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_map_1to10combinedVarEnergySCFrame are pixel map data from all
directions (omnidirectional) in Var Energy SC Frame, no CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_NOCG_SP_RAM_1YR doi:10.48322/gre9-7z41
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1 year-cadence) IBEX-Hi map data for the
years 2009-2013 in the form of ram-directionl ENA (hydrogen) fluxes with no
Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
with correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_yearN for N=1,5, includes pixel map data from ram direction
(ram-directional), no CG, SP, 1 year cadence. 
Modification History
The Release 7 data extend through Map 10 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R07_NOCG_SP_RAM_VESCF_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 7 (1-to-5-year-average) IBEX-Hi map data
for the years 2009-2014 in the form of ram-directional ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and correction (sp) for ENA survival probability in Var Energy SC Frame between
1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mif = Mono Inertial Frame 
veif = Var Energy Inertial Frame 
vescf = Var Energy SC Frame 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_year_1to5combinedVarEnergySCFrame are pixel map data
antiram-directional in Var Energy SC Frame, no CG, SP, 5 year cadence. 
Modification History
The Release 7 data extend through Maps 1-10. The present CDF data set was
converted from the originally archived data in ascii list format but otherwise
includes no changes in the data. The original data are given in 30 rows for
Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East Longitude. The
accompanying documentation described the row latitude data as starting from the
north Ecliptic pole (+90 degrees) and decreasing in value to the south Ecliptic
pole (-90 degrees). During preparation of the data set in CDF format, SPDF
discovered that the correct order was increasing from row 1 for the South
Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is defined
correctly for the column order but we have instead used west longitude to better
represent the outward-looking viewpoint from IBEX to the outer heliosphere as
typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS-GAL_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional ENA (hydrogen) fluxes between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f2-ribbonMapsGAL includes f2 ribbon
pixel map data from all directions (omnidirectional), 5 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS-J2000_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional ENA (hydrogen) fluxes between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f2-ribbonMapsJ2000 includes f2
ribbon pixel map data from all directions (omnidirectional), 5 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
Back to top
IBEX_H3_ENA_HI_R08_OMNI_F2-RIBBON-MAPS_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional ENA (hydrogen) fluxes between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f2-ribbonMaps includes f2 ribbon
pixel map data from all directions (omnidirectional), 5 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
Back to top
IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS-GALACTIC_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional GDF (Globally Distributed Flux)
ENA (hydrogen) fluxes between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
gdf = Globally Distributed Flux. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f3-gdfGALACTIC includes f3 GDF
(Globally Distributed Flux) pixel map data from all directions
(omnidirectional), 5 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
Back to top
IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS-J2000_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional GDF (Globally Distributed Flux)
ENA (hydrogen) fluxes between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
gdf = Globally Distributed Flux. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f3-gdfJ2000 includes f3 GDF
(Globally Distributed Flux) pixel map data from all directions
(omnidirectional), 5 year cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R08_OMNI_F3-GDF-MAPS_5YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 8 IBEX-Hi map data for the years 2009-2014
(5 year-cadence) in the form of omnidirectional GDF (Globally Distributed Flux)
ENA (hydrogen) fluxes between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
gdf = Globally Distributed Flux. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the f3-gdfmaps includes f3 GDF (Globally
Distributed Flux) pixel map data from all directions (omnidirectional), 5 year
cadence. 
Modification History
The latest Release 16 data extend through Map 22 and contain modications and
updates of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from
Release 7, maps 1-14 from Release 10, maps 15-22 from Release 16. The present
CDF data set was converted from the originally archived data in ascii list
format but otherwise includes no changes in the data. The original data are
given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic
East Longitude. The accompanying documentation described the row latitude data
as starting from the north Ecliptic pole (+90 degrees) and decreasing in value
to the south Ecliptic pole (-90 degrees). During preparation of the data set in
CDF format, SPDF discovered that the correct order was increasing from row 1 for
the South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R10_CG_NOSP_ANTIRAM_1YR doi:10.48322/8960-pv55
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of antiram-direction fluxes with corrections
for spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_yearN for N=1,7, includes pixel map data from antiram
direction, CG, noSP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_NOSP_ANTIRAM_7YR doi:10.48322/9g82-sm34
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of antiram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_ single, includes pixel map data from antiram direction,
CG, noSP, 7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_NOSP_OMNI_6MO doi:10.48322/3v75-8m19
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (6 months-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, with multiple versions of data sets including
no corrections, full corrections for spacecraft  motion, and corrections for ENA
survival probability between 1 and 100 AU. 
3: The data consist of all-sky maps in Solar West Ecliptic angles of ENA
(hydrogen) fluxes from IBEX-Hi energy bands 2-6 in numerical data form. Energy
channels 2-6 have FWHM ranges of 0.52-0.95, 0.84-1.55, 1.36-2.50, 1.99-3.75,
3.13-6.00 keV, respectively. The corresponding center-point energies are 0.71,
1.11, 1.74, 2.73, and 4.29 keV. Details of the data and enabled science from
Release 10 are given in the following journal publication: 
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6: cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
7: nocg = no Compton-Getting corrections 
8: sp = survival probability corrections have been applied to the data to
account for the loss of ENAs due to radiation pressure, photoionization and
ionization via charge exchange with solar wind protons as they stream through
the heliosphere. This correction scales the data out from IBEX at 1 AU to ~100
AU. In the original data this mode is denoted as Tabular. 
9: noSP - no survival probability corrections have been applied to the data. 
10: omni = data from all directions. 
11: ram = data was collected when the spacecraft was ramming into the incoming
ENAs. 
12: antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
13: The following list associates Release 10 map numbers (1-14) with mission
year (1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015). 
14: Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
15: Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
16: Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
17: Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
18: Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
19: Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
20: Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
21: Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
22: Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
23: Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
24: Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
25: Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
26: Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
27: Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
28: This particular data set, denoted in the original ascii files as
hvset_cg_mapN for N=1,14, includes pixel map data from all directions
(omnidirectional), CG, no SP, 6 month cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_NOSP_OMNI_7YR doi:10.48322/68kk-mv11
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of omni-direction fluxes with corrections for spacecraft
motion (cg: Compton-Getting) but with no corrections (sp) for ENA survival
probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as hvset_cg_
single, includes pixel map data from omni direction, CG, noSP, 7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R10_CG_NOSP_RAM_1YR doi:10.48322/0f8a-vp56
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of ram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_yearN for N=1,7, includes pixel map data from RAM direction
(ram-direction), CG, noSP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_NOSP_RAM_7YR doi:10.48322/fgm0-nz35
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of ram-direction fluxes with corrections for spacecraft
motion (cg: Compton-Getting) but with no corrections (sp) for ENA survival
probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_ single, includes pixel map data from ram direction, CG, noSP,
7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_SP_ANTIRAM_1YR doi:10.48322/yzz4-et03
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (1-year-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, in the form of anti-RAM-directional fluxes
with corrections for spacecraft motion (cg: Compton-Getting) and with
corrections (sp) for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_yearN for N=1,7, includes pixel map data from antiRAM
direction (antiRAMdirectional), CG, SP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_SP_ANTIRAM_7YR doi:10.48322/aszx-jt19
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of antiram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) and with corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_single, includes pixel map data from antiram direction,
CG,SP, 7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_SP_OMNI_6MO doi:10.48322/jq00-4j33
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (6 months-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, in the form of omnidirectional fluxes with
corrections (cg) for spacecraft motion (Compton-Getting) and corrections (sp)
for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015): 
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_mapN for N=1,14, includes pixel map data from all directions
(omnidirectional), CG, SP, 6 month cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_SP_OMNI_7YR doi:10.48322/bcjj-r065
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of omni-direction fluxes with corrections for spacecraft
motion (cg: Compton-Getting) and with corrections (sp) for ENA survival
probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_ single, includes pixel map data from omni direction, CG,SP, 7
year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R10_CG_SP_RAM_1YR doi:10.48322/a4bm-9844
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (1-year-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, in the form of RAM-directional fluxes with
corrections for spacecraft motion (cg: Compton-Getting) and with corrections
(sp) for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_yearN for N=1,7, includes pixel map data from RAM direction
(RAMdirectional), CG, SP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_CG_SP_RAM_7YR doi:10.48322/nqsx-9a30
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of ram-direction fluxes with corrections for spacecraft
motion (cg: Compton-Getting) and with corrections (sp) for ENA survival
probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_single, includes pixel map data from ram direction, CG,SP,
7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_NOSP_ANTIRAM_1YR doi:10.48322/mfpx-sd13
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of antiram-direction fluxes with no
corrections for spacecraft motion (nocg: no Compton-Getting) and with no
corrections (nosp) for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_yearN for N=1,7, includes pixel map data from antiram
direction, CG, noSP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_NOSP_ANTIRAM_7YR doi:10.48322/s5jq-td10
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of antiram-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) and with no corrections (nosp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_single, includes pixel map data from antiram direction, noCG,
noSP, 7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_NOSP_OMNI_6MO doi:10.48322/va6f-mg80
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (6 months-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, in the form of omnidirectional fluxes without
any corrections (nocg) for spacecraft motion (Compton-Getting) and ENA survival
probability (nosp) between 1 and 100 AU.
3: The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015): 
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as hvset_mapN
for N=1,14, includes pixel map data from all directions (omnidirectional), no
CG, no SP, 6 month cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_NOSP_OMNI_7YR doi:10.48322/redf-vj78
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of omni-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) and with no corrections (nosp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_single, includes pixel map data from omni direction, noCG, noSP, 7 year
cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_NOSP_RAM_1YR doi:10.48322/ab6p-7w38
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of ram-direction fluxes with no corrections
for spacecraft motion (nocg: no Compton-Getting) and with no corrections (nosp)
for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_yearN for N=1,7, includes pixel map data from antiram direction,
CG, noSP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_SP_ANTIRAM_1YR doi:10.48322/83y1-pw33
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of antiram-direction fluxes with no
corrections for spacecraft motion (nocg: no Compton-Getting) and with
corrections (sp) for ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_noSP_antiram_yearN for N=1,7, includes  pixelmap data from anti
ramdirection, noCG, SP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_SP_ANTIRAM_7YR doi:10.48322/bnb2-z378
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of antiram-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) but with corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_single, includes pixel map data from antiram direction,
noCG, SP, 7 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_SP_OMNI_6MO doi:10.48322/jm1t-pg27
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 (6 months-cadence) IBEX-Hi map data for
the first seven years, 2009-2015, with multiple versions of data sets including
no corrections, full corrections for spacecraft  motion, and corrections for ENA
survival probability between 1 and 100 AU. 
3: The data consist of all-sky maps in Solar West Ecliptic angles of ENA
(hydrogen) fluxes from IBEX-Hi energy bands 2-6 in numerical data form. Energy
channels 2-6 have FWHM ranges of 0.52-0.95, 0.84-1.55, 1.36-2.50, 1.99-3.75,
3.13-6.00 keV, respectively. The corresponding center-point energies are 0.71,
1.11, 1.74, 2.73, and 4.29 keV. Details of the data and enabled science from
Release 10 are given in the following journal publication: 
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6: cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
7: nocg = no Compton-Getting corrections 
8: sp = survival probability corrections have been applied to the data to
account for the loss of ENAs due to radiation pressure, photoionization and
ionization via charge exchange with solar wind protons as they stream through
the heliosphere. This correction scales the data out from IBEX at 1 AU to ~100
AU. In the original data this mode is denoted as Tabular. 
9: noSP - no survival probability corrections have been applied to the data. 
10: omni = data from all directions. 
11: ram = data was collected when the spacecraft was ramming into the incoming
ENAs. 
12: antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
13: The following list associates Release 10 map numbers (1-14) with mission
year (1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015). 
14: Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
15: Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
16: Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
17: Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
18: Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
19: Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
20: Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
21: Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
22: Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
23: Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
24: Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
25: Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
26: Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
27: Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
28: This particular data set, denoted in the original ascii files as
hvset_tabular_mapN for N=1,14, includes pixel map data from all directions
(omnidirectional), no CG, SP, 6 month cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_SP_OMNI_7YR doi:10.48322/24kn-z991
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 seven-year IBEX-Hi map data for
2009-2015, in the form of omni-direction fluxes with no corrections for
spacecraft motion (nocg: Compton-Getting) but with corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_single, includes pixel map data from omni direction, noCG, noSP, 7
year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R10_NOCG_SP_RAM_1YR doi:10.48322/3f2m-z528
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2017. 
2: This data set is from the Release 10 one-year IBEX-Hi map data for the first
seven years, 2009-2015, in the form of ram-direction fluxes with no corrections
for spacecraft motion (nocg: no Compton-Getting) and with corrections (sp) for
ENA survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 10 map numbers (1-14) with mission year
(1-7), orbits (11-310b), and dates (12/25/2008-12/23/2015); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
8: This particular data set, denoted in the original ascii files as
hvset_tabular_noSP_ram_yearN for N=1,7, includes  pixelmap data from
ramdirection, noCG, SP, 1 year cadence. 
Modification History
The Release 10 data extend through Map 14 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R12_MAGNETOSPHERE_24MIN doi:10.48322/00z8-0d49
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2018. 
2: This data set is from the IBEX-Hi Release 12 Count Data for Magnetospheric
Imaging. This release provides data for various IBEX orbits from 23 (2009-03-26)
to 207b (2013-05-30). The data include 21 orbits from IBEX-Hi 6-degree histogram
ENA count data, which is primarily what have been used in IBEX magnetospheric
studies.
3. The data consist of IBEX-Hi Count Data for Magnetospheric Imaging during
instrument pointing in spin angle 0 - 360 degrees between the north and south
Ecliptic poles. Spin angle zero corresponds to the north Ecliptic pole. Counts
come from IBEX-Hi energy bands 2-6 in numerical data form corresponding to
energy bins 2-6: 2) ~0.71, 3) ~1.11, 4) ~1.74, 5) ~2.73, 6) ~4.3 keV. Background
counts have not been removed. Counts are separated into 6-degree latitudinal
bins, with each # angle label representing the center of the bin. Details of the
data and enabled science from Release 12 are given in the following journal
publications: McComas et al. 2011,2012b; Fuselier et al. 2010, 2015; Petrinec et
al. 2011; Ogasawara et al. 2013, 2019; and Dayeh et al. 2015Data Location:
http://ibex.swri.edu/ibexpublicdata/Data_Release_12/index.htmlContact: Maher
Dayeh, Southwest Research Institute, San Antonio, TX maldayeh@swri.edu 
Orbit Start and End Times:
23: 2009-03-26 21:09:00.318 to 2009-04-03 16:07:51.743
24: 2009-04-03 12:10:21.253 to 2009-04-11 08:15:09.669
25: 2009-04-11 05:06:40.967 to 2009-04-18 22:05:11.125
27: 2009-04-26 08:27:40.916 to 2009-05-04 05:31:06.519
28: 2009-05-04 02:02:57.673 to 2009-05-11 21:13:47.596
29: 2009-05-11 17:27:02.484 to 2009-05-19 19:27:18.831
51: 2009-10-26 08:19:34.905 to 2009-11-03 02:38:01.730
52: 2009-11-02 22:34:07.792 to 2009-11-10 19:03:55.230
53: 2009-11-10 15:46:22.161 to 2009-11-18 10:58:17.674
55: 2009-11-25 23:44:19.069 to 2009-12-03 11:26:37.151
56: 2009-12-03 08:22:31.792 to 2009-12-10 22:03:52.604
57: 2009-12-10 18:55:33.969 to 2009-12-18 06:58:47.247
72: 2010-04-04 11:17:28.386 to 2010-04-12 09:13:51.008
74: 2010-04-19 14:09:01.851 to 2010-04-27 03:44:14.913
77: 2010-05-12 01:33:51.796 to 2010-05-19 20:43:01.583
78: 2010-05-19 17:33:48.047 to 2010-05-27 13:02:03.396
103: 2010-11-26 07:56:05.324 to 2010-12-04 04:11:44.879
187a: 2012-11-21 00:17:13.430 to 2012-11-25 00:40:26.707
188b: 2012-12-03 12:46:18.859 to 2012-12-08 00:44:50.846
206a: 2013-05-13 23:15:27.433 to 2013-05-17 12:19:58.215
207b: 2013-05-26 12:21:08.868 to 2013-05-30 23:14:44.989
For the first two and a half years of science operations (through Orbit 127),
IBEX's orbital period was ~7.5 days and the spin axis was repointed once each
orbit (around perigee), leading to bands of sky viewing centered 7.5 apart. In
June 2011, over Orbits 128 and 129, IBEX was maneuvered into a previously
unknown, long-term stable lunar synchronous orbit with apogee still ~50 RE
(McComas et al. 2011a). Since then, IBEX's orbital period has been ~9.1 days
(one-third of the lunar sidereal period of 27.3 days). Orbit numbers from 130
onward are split into two segments, 'a' and 'b'. Furthermore, starting in orbit
segment 184a, the IBEX team modified the IBEX-Hi energy step sequence and
eliminated the lowest energy step (ESA1) in exchange for doubling the
statistical sampling of ESA3 (center energy ~1.1 keV).
Modification History
The IBEX Release 12 data 
 
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IBEX_H3_ENA_HI_R13_CG_NOSP_ANTIRAM_1YR doi:10.48322/9vdf-1a43
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2018. 
2: This data set is from the Release 13 one-year IBEX-Hi map data for the nine
years, 2009-2018, in the form of antiram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 13 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 13 map numbers (1-20) with mission year
(1-10), orbits (11-431bb), and dates (12/25/2008-12/26/2018); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: year 8, orbits 311a-330b, dates 12/24/2015-06/23/2016
Map 16: year 8, orbits 331a-351a, dates 06/24/2016-12/26/2016
Map 17: year 9, orbits 351b-371a, dates 12/26/2016-06/25/2017
Map 18: year 9, orbits 371b-391a, dates 06/25/2017-12/25/2017
Map 19: year 10, orbits 391a-411b, dates 12/25/2017-06/28/2018
Map 20: year 10, orbits 412a-431b, dates 06/29/2018-12/26/2018
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_yearN for N=8, includes pixel map data from antiram
direction, CG, noSP, 1 year cadence. 
Modification History
The Release 13 data extend through Map 20 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R13_CG_NOSP_RAM_1YR doi:10.48322/jr67-ar66
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 14
releases of IBEX-HI and/or IBEX-LO data covering 2009-2018. 
2: This data set is from the Release 13 one-year IBEX-Hi map data for the nine
years, 2009-2018, in the form of ram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU.  
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 13 map numbers (1-20) with mission year
(1-10), orbits (11-431bb), and dates (12/25/2008-12/26/2018); each year is
associated with two consecutive maps;
Map 1: year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: year 8, orbits 311a-330b, dates 12/24/2015-06/23/2016
Map 16: year 8, orbits 331a-351a, dates 06/24/2016-12/26/2016
Map 17: year 9, orbits 351b-371a, dates 12/26/2016-06/25/2017
Map 18: year 9, orbits 371b-391a, dates 06/25/2017-12/25/2017
Map 19: year 10, orbits 391a-411b, dates 12/25/2017-06/28/2018
Map 20: year 10, orbits 412a-431b, dates 06/29/2018-12/26/2018
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_yearN for N=8, includes pixel map data from antiram direction,
CG, noSP, 1 year cadence. 
Modification History
The Release 13 data extend through Map 20 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7.
The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R14_PRESS-SLOPE_CG_NOSP_RAM_3YR doi:10.48322/ayqx-a052
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 15
releases of IBEX-HI and/or IBEX-LO data covering 2009-2018. 
2: This data set is derived from the Release 14 three-year IBEX-Hi map data with
two-year overlaps to adjacent maps, 2009-2011, 2010-2012, 2011-2013, and so
forth through 2015-2017 from ram-direction fluxes with corrections for
spacecraft motion (cg: Compton-Getting) but with no corrections (sp) for ENA
survival probability between 1 and 100 AU. The data set parameters include
line-of-sight (LOS) integrated pressures separately computed from the Global
Distributed Flux (GDF), the ribbon flux, and the total of both LOS pressures.
Additionally there are signal/noise ratios for the GDF, ribbon, and total
pressures. Finally, there are power-law slope and values for the GDF
differential flux, also including signal/noise of the slope.  
3: The data consist of ram-direction sky maps in Solar Ecliptic Longitude (east
and west) and Latitude angles for the above parameters. 
4: Details of the data and enabled science from Release 14 are given in the
following journal publication: Schwadron, N. A., et al. (2018), Time Dependence
of the IBEX Ribbon and the Globally Distributed Energetic Neutral Atom Flux
Using the First 9 Years of Observations
https://iopscience.iop.org /article/10.3847/1538-4365/aae48e/meta
5: The following codes are used to define dataset types in the multiple IBEX
data releases:  
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
6: This particular dataset denoted in the original ascii files as:
-- GDFPressure: Globally Distributed Flux Line-of-Sight Integrated Pressure in
pdyne-au/cm^2
-- GDFSlope: Power-Law Slope of the differential flux spectrum for the Globally
Distributed Flux
-- GDFSlopeSN: Signal/Noise ratio of the GDF differential flux power-law slope
where noise represents uncertainty 
-- GDFSN: Globally Distributed Flux Signal/Noise, where Noise is defined as the
uncertainty and the Signal is GDF Line-of-Sight -integrated pressure
-- RibbonPressure: Ribbon Line-of-Sight Integrated Pressure in pdyne-au/cm^2
-- RibbonSN: Ribbon Signal/Noise, where Noise is defined as the uncertainty and
the Signal is GDF  Line-of-Sight -integrated pressure
-- TotPressure: Total Pressure in ENA maps including both the GDF and Ribbon.
Line-of-Sight Integrated Pressure in pdyne-au/cm^2
-- TotSN: Total Pressure Signal-to-Noise where noise represents uncertainty and
signal represents the total LOS-integrated pressure
Modification History
The Release 14 data extend through Map 20 and contain modifications and updates
of Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release
7. The present CDF data set was converted from the originally archived data in
ascii list format but otherwise includes no changes in the data. The original
data are given in 30 rows for Solar Ecliptic Latitude and 60 columns for Solar
Ecliptic East Longitude. The accompanying documentation described the row
latitude data as starting from the north Ecliptic pole (+90 degrees) and
decreasing in value to the south Ecliptic pole (-90 degrees). During preparation
of the data set in CDF format, SPDF discovered that the correct order was
increasing from row 1 for the South Ecliptic pole to row 30 for the north
Ecliptic pole. East longitude is defined correctly for the column order but we
have instead used west longitude to better represent the outward-looking
viewpoint from IBEX to the outer heliosphere as typically used in IBEX team
plots. 
 
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IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_1YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 15 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes with
no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
no correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
ribcen = maps are in a ribbon centered frame. 
7. The following list associates Release 15 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: Data Release 15 description:  Maps are in a ribbon centered frame. Data are
Compton-Getting and Survival Probability corrected.  Centers for different
energies are as follows (following Funsten et al. 2013): 
 Map Centers for each energy (in eclipticJ2000; [lon,lat]): 
 ESA2 ribbon center : b_lon_lat_ec = [218.5, 43.1] 
 ESA3 ribbon center : b_lon_lat_ec = [220.3, 40.5] 
 ESA4 ribbon center : b_lon_lat_ec = [219.6, 39.8] 
 ESA5 ribbon center : b_lon_lat_ec = [217.9, 37.7] 
 ESA6 ribbon center : b_lon_lat_ec = [214.2, 32.4] 
9: This particular data set, denoted in the original ascii files as
ribcen_esaN_hvset_tabular_cg_YYYY for N=2-6, and YYYY = 2009-2017, includes
pixel map data from ribbon centered frame, CG, SP, 1 year cadence.
Modification History
The Release 15 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_2YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 15 (2 or 3 year-cadence) IBEX-Hi map data
for the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and no correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
ribcen = maps are in a ribbon centered frame. 
Combined maps information: years01-03 refers to 2009, 2010, 2011  years04-05
refers to 2012, 2013;  years06-07 refers to 2014, 2015;  years08-09 refers to
2016, 2017. 
7. The following list associates Release 15 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: Data Release 15 description:  Maps are in a ribbon centered frame. Data are
Compton-Getting and Survival Probability corrected.  Centers for different
energies are as follows (following Funsten et al. 2013): 
 Map Centers for each energy (in eclipticJ2000; [lon,lat]): 
 ESA2 ribbon center : b_lon_lat_ec = [218.5, 43.1] 
 ESA3 ribbon center : b_lon_lat_ec = [220.3, 40.5] 
 ESA4 ribbon center : b_lon_lat_ec = [219.6, 39.8] 
 ESA5 ribbon center : b_lon_lat_ec = [217.9, 37.7] 
 ESA6 ribbon center : b_lon_lat_ec = [214.2, 32.4] 
9: This particular data set, denoted in the original ascii files as
ribcen_esa2_hvset_tabular_cg_single_yearsYYY for YYY = 123 refers to 2009, 2010,
2011; YYY = 45 refers to 2012, 2013; YYY = 67 refers to 2014, 2015; YYY = 89
refers to 2016, 2017; For instance, ribcen_esa5_hvset_tabular_cg_single_years45
contains data for combined years 2012 and 2013 at ESA 5. The set includes pixel
map data from ribbon centered frame, CG, SP, 2 or 3 year cadence.
Modification History
The Release 15 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R15_CG_SP_RIBCEN_3YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 15 (2 or 3 year-cadence) IBEX-Hi map data
for the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes
with no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion
and no correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
ribcen = maps are in a ribbon centered frame. 
Combined maps information: years01-03 refers to 2009, 2010, 2011  years04-05
refers to 2012, 2013;  years06-07 refers to 2014, 2015;  years08-09 refers to
2016, 2017. 
7. The following list associates Release 15 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: Data Release 15 description:  Maps are in a ribbon centered frame. Data are
Compton-Getting and Survival Probability corrected.  Centers for different
energies are as follows (following Funsten et al. 2013): 
 Map Centers for each energy (in eclipticJ2000; [lon,lat]): 
 ESA2 ribbon center : b_lon_lat_ec = [218.5, 43.1] 
 ESA3 ribbon center : b_lon_lat_ec = [220.3, 40.5] 
 ESA4 ribbon center : b_lon_lat_ec = [219.6, 39.8] 
 ESA5 ribbon center : b_lon_lat_ec = [217.9, 37.7] 
 ESA6 ribbon center : b_lon_lat_ec = [214.2, 32.4] 
9: This particular data set, denoted in the original ascii files as
ribcen_esa2_hvset_tabular_cg_single_yearsYYY for YYY = 123 refers to 2009, 2010,
2011; YYY = 45 refers to 2012, 2013; YYY = 67 refers to 2014, 2015; YYY = 89
refers to 2016, 2017; For instance, ribcen_esa5_hvset_tabular_cg_single_years45
contains data for combined years 2012 and 2013 at ESA 5. The set includes pixel
map data from ribbon centered frame, CG, SP, 2 or 3 year cadence.
Modification History
The Release 15 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_11YR doi:10.48322/y9dn-wh12
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11-year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_antiram_cg_single includes pixel map data from antiram direction
(antiram-directional), CG, NOSP, 11 year cadence. 
 
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IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_1YR doi:10.48322/g1tq-ea69
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_antiram_cg_N for N=2009,2019, includes pixel map data from antiram
direction (antiram-directional), CG, NOSP, 1 year cadence. 
 
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IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft motion and
no correction for ENA survival probability (nosp) mono-energy (mono) between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_single\hv60.hide-trp-mono_80-M-V , where M = 0.71, 1.11,
1.74, 2.73,  4.29 showing the energy of the channel, and V = 'flux', 'fvar', or
'fsnr', includes pixel map data from antiram direction, CG, no SP, mono-energy,
11 year cadence.
 
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IBEX_H3_ENA_HI_R16_CG_NOSP_ANTIRAM_MONO_1YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft motion and
no correction for ENA survival probability (nosp) mono-energy (mono) between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_cg_N\hv60.hide-trp-mono_80-M-V , where N=2009,2019, M = 0.71,
1.11, 1.74, 2.73,  4.29 showing the energy of the channel, and V = 'flux',
'fvar', or 'fsnr', includes pixel map data from antiram direction, CG, no SP,
mono-energy, 1 year cadence.
 
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IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_11YR doi:10.48322/r428-6n89
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of omnidirectional ENA (hydrogen) fluxes with Compton-Getting
correction (cg) of flux spectra for spacecraft  motion and no correction (nosp)
for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_single, includes pixel map data from all directions (omnidirectional),
CG, no SP, 11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_6MO doi:10.48322/wfbs-w642
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction (nosp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as hvset_cg_NX
for N=2009,2019, which indicates a year data collected, and X = A or B, showing
first or second half of the year, includes pixel map data from all directions
(omnidirectional), CG, no SP, 6 month cadence. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data
averaged for the years 2009-2019 in the form of omnidirectional ENA (hydrogen)
fluxes with Compton-Getting correction (cg) of flux spectra for spacecraft 
motion and no correction (nosp) for ENA survival probability between 1 and 100
AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_single/hv60.hide-trp-mono_80-m-v, where m = 0.71, 1.11, 1.74, 2.73, or
4.29 showing the energy of the channel, and v = 'flux', 'fvar', or 'fsnr',
includes pixel map data from all directions (omnidirectional), CG, no SP,
mono-energy, 11 year cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_NOSP_OMNI_MONO_6MO
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) mono-energy (mono) between 1 and
100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_NX/hv60.hide-trp-mono_80-m-v, where N=2009 - 2019, which indicates a
year data collected, and X = A or B, showing first or second half of the year, m
= 0.71, 1.11, 1.74, 2.73, or 4.29 showing the energy of the channel, and v =
'flux', 'fvar', or 'fsnr', includes pixel map data from all directions
(omnidirectional), CG, NOSP, mono-energy, 6 month cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_11YR doi:10.48322/30g5-mx06
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of ram-directional ENA (hydrogen) fluxes with Compton-Getting
correction (cg) of flux spectra for spacecraft  motion and no correction for ENA
survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_single, includes pixel map data from ram direction, CG, no SP,
11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_1YR doi:10.48322/qet6-1611
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and no
correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_N for N=2009,2019, includes pixel map data from ram direction
(ram-directional), CG, no SP, 1 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of ram-directional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft motion and no
correction for ENA survival probability (nosp) mono-energy (mono) between 1 and
100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_single\hv60.hide-trp-mono_80-M-V , where M = 0.71, 1.11, 1.74,
2.73,  4.29 showing the energy of the channel, and V = 'flux', 'fvar', or
'fsnr', includes pixel map data from ram direction, CG, no SP, mono-energy, 11
year cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_NOSP_RAM_MONO_1YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of ram-directional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft motion and no
correction for ENA survival probability (nosp) mono-energy (mono) between 1 and
100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_ram_cg_N\hv60.hide-trp-mono_80-M-V , where N=2009,2019, M = 0.71,
1.11, 1.74, 2.73,  4.29 showing the energy of the channel, and V = 'flux',
'fvar', or 'fsnr', includes pixel map data from antiram direction, CG, no SP,
mono-energy, 1 year cadence.
 
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IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_11YR doi:10.48322/qc27-hw91
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of antiram-directional ENA (hydrogen) fluxes with Compton-Getting
correction (cg) of flux spectra for spacecraft  motion and correction for ENA
survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_single, includes pixel map data from antiram direction,
CG, SP, 11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_1YR doi:10.48322/ww5n-ty58
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_N for N=2009,2019, includes pixel map data from antiram
direction (antiram-directional), CG, SP, 1 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data
averaged for the years 2009-2019 in the form of ANTIRAMdirectional ENA
(hydrogen) fluxes with Compton-Getting correction (cg) of flux spectra for
spacecraft  motion and correction for ENA survival probability (sp) between 1
and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_single/hv60.hide-trp-mono_80-m-v, where m = 0.71, 1.11, 1.74,
2.73, or 4.29 showing the energy of the channel, and v = 'flux', 'fvar', or
'fsnr', includes pixel map data from ANTIRAM direction (ANTIRAMdirectional), CG,
SP, mono-energy, 11 year cadence.
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_SP_ANTIRAM_MONO_1YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directional ENA (hydrogen) fluxes
with Compton-Getting correction (cg) of flux spectra for spacecraft motion and
correction for ENA survival probability (sp) mono-energy (mono) between 1 and
100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_antiram_cg_N\hv60.hide-trp-mono_80-M-V , where N=2009,2019, M =
0.71, 1.11, 1.74, 2.73,  4.29 showing the energy of the channel, and V = 'flux',
'fvar', or 'fsnr', includes pixel map data from antiram direction, CG, SP,
mono-energy, 1 year cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_11YR doi:10.48322/pjt4-pe60
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of omnidirectional ENA (hydrogen) fluxes with Compton-Getting
correction (cg) of flux spectra for spacecraft  motion and correction (sp) for
ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_single, includes pixel map data from all directions
(omnidirectional), CG, SP, 11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_2YR doi:10.48322/6181-nk59
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
(2 year-cadence) in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_single_Nyears, where N = 2 or 3, shows number of years of
averaging, includes pixel map data from all directions (omnidirectional), CG,
SP, 2 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_3YR doi:10.48322/m780-tm05
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
(3 year-cadence) in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction (sp) for ENA survival probability between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_single_Nyears, where N = 2 or 3, shows number of years of
averaging, includes pixel map data from all directions (omnidirectional), CG,
SP, 3 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_6MO doi:10.48322/f50h-6551
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_NX for N=2009,2019, which indicates a year data collected, and
X = A or B, showing first or second half of the year, includes pixel map data
from all directions (omnidirectional), CG, SP, 6 month cadence. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data
averaged for the years 2009-2019 in the form of omnidirectional ENA (hydrogen)
fluxes with Compton-Getting correction (cg) of flux spectra for spacecraft 
motion and correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_single/hv60.hide-trp-mono_80-m-v, where m = 0.71, 1.11, 1.74,
2.73, or 4.29 showing the energy of the channel, and v = 'flux', 'fvar', or
'fsnr', includes pixel map data from all directions (omnidirectional), CG, SP,
mono-energy, 11 year cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_OMNI_MONO_6MO
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (6 months-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of omnidirectional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp)mono-energy (mono) between 1 and 100
AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_NX/hv60.hide-trp-mono_80-m-v, where N=2009 - 2019, which
indicates a year data collected, and X = A or B, showing first or second half of
the year, m = 0.71, 1.11, 1.74, 2.73, or 4.29 showing the energy of the channel,
and v = 'flux', 'fvar', or 'fsnr', includes pixel map data from all directions
(omnidirectional), CG, SP, mono-energy, 6 month cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_CG_SP_RAM_11YR doi:10.48322/b2ht-5g89
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of ram-directional ENA (hydrogen) fluxes with Compton-Getting
correction (cg) of flux spectra for spacecraft  motion and correction for ENA
survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_single, includes pixel map data from ram direction, CG, SP,
11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
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IBEX_H3_ENA_HI_R16_CG_SP_RAM_1YR doi:10.48322/6kb9-t215
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of ram-directionl ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft  motion and
correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_N for N=2009,2019, includes pixel map data from ram
direction (ram-directional), CG, SP, 1 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_SP_RAM_MONO_11YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (11 year-cadence) IBEX-Hi map data
averaged for the years 2009-2019 in the form of RAMdirectional ENA (hydrogen)
fluxes with Compton-Getting correction (cg) of flux spectra for spacecraft 
motion and correction for ENA survival probability (sp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_cg_tabular_single/hv60.hide-trp-mono_80-m-v, where m = 0.71, 1.11, 1.74,
2.73, or 4.29 showing the energy of the channel, and v = 'flux', 'fvar', or
'fsnr', includes pixel map data from RAM direction (RAMdirectional), CG, SP,
mono-energy, 11 year cadence.
 
Dataset in CDAWeb
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IBEX_H3_ENA_HI_R16_CG_SP_RAM_MONO_1YR
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of ram-directional ENA (hydrogen) fluxes with
Compton-Getting correction (cg) of flux spectra for spacecraft motion and
correction for ENA survival probability (sp) mono-energy (mono) between 1 and
100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
mono = mono-energy Compton-Getting corrected maps. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_tabular_ram_cg_N\hv60.hide-trp-mono_80-M-V , where N=2009,2019, M = 0.71,
1.11, 1.74, 2.73,  4.29 showing the energy of the channel, and V = 'flux',
'fvar', or 'fsnr', includes pixel map data from ram direction, CG, SP,
mono-energy, 1 year cadence.
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_NOCG_NOSP_ANTIRAM_11YR doi:10.48322/tvjy-cp94
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 IBEX-Hi map data for the years 2009-2019
in the form of antiram-directional ENA (hydrogen) fluxes with no Compton-Getting
correction (nocg) of flux spectra for spacecraft  motion and no correction for
ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_single, includes pixel map data from antiram direction, no
CG, no SP, 11 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots. 
 
Dataset in CDAWeb
Data Access Code Examples written in Python and IDL®.
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IBEX_H3_ENA_HI_R16_NOCG_NOSP_ANTIRAM_1YR doi:10.48322/xrpe-jx49
Description
1: The Interstellar Boundary Explorer (IBEX) has operated in space since 2008
updating our knowledge of the outer heliosphere and its interaction with the
local interstellar medium. Start-time: 2008-12-25. There are currently 16
releases of IBEX-HI and/or IBEX-LO data covering 2009-2019. 
2: This data set is from the Release 16 (1 year-cadence) IBEX-Hi map data for
the years 2009-2019 in the form of antiram-directionl ENA (hydrogen) fluxes with
no Compton-Getting correction (nocg) of flux spectra for spacecraft  motion and
no correction for ENA survival probability (nosp) between 1 and 100 AU. 
3. The data consist of all-sky maps in Solar Ecliptic Longitude (east and west)
and Latitude angles for ENA (hydrogen) fluxes from IBEX-Hi energy bands 2-6 in
numerical data form. Energy channels 2-6 have FWHM ranges of 0.52-0.95,
0.84-1.55, 1.36-2.50, 1.99-3.75, 3.13-6.00 keV, respectively. The corresponding
center-point energies are 0.71, 1.11, 1.74, 2.73, and 4.29 keV. Details of the
data and enabled science from Release 10 are given in the following journal
publication:
4: McComas, D. J., et al. (2017), Seven Years of Imaging the Global Heliosphere
with IBEX, Astrophys. J. Supp. Ser., 229(2), 41 (32 pp.), 
5: http://doi.org/10.3847/1538-4365/aa66d8  
6. The following codes are used to define dataset types:
cg = Compton-Getting corrections have been applied to the data to account for
the speed of the spacecraft relative to the direction of arrival of the ENAs. 
nocg = no Compton-Getting corrections 
sp = survival probability corrections have been applied to the data to account
for the loss of ENAs due to radiation pressure, photoionization and ionization
via charge exchange with solar wind protons as they stream through the
heliosphere. This correction scales the data out from IBEX at 1 AU to ~100 AU.
In the original data this mode is denoted as Tabular. 
noSP - no survival probability corrections have been applied to the data. 
omni = data from all directions. 
ram = data was collected when the spacecraft was ramming into the incoming ENAs.
antiram = data was collected when the spacecraft was moving away from the
incoming ENAs. 
7. The following list associates Release 16 map numbers (1-22) with mission year
(1-9), orbits (11-471b), and dates (12/25/2008-12/26/2019): 
Map 1: Map2009A, year 1, orbits 11-34, dates 12/25/2008-06/25/2009
Map 2: Map2009B, year 1, orbits 35-58, dates 06/25/2009-12/25/2009
Map 3: Map2010A, year 2, orbits 59-82, dates 12/25/2009-06/26/2010
Map 4: Map2010B, year 2, orbits 83-106, dates 06/26/2010-12/26/2010
Map 5: Map2011A, year 3, orbits 107-130a, dates 12/26/2010-06/25/2011
Map 6: Map2011B, year 3, orbits 130b-150a, dates 06/25/2011-12/24/2011
Map 7: Map2012A, year 4, orbits 150b-170a, dates 12/24/2011-06/22/2012
Map 8: Map2012B, year 4, orbits 170b-190b, dates 06/22/2012-12/26/2012
Map 9: Map2013A, year 5, orbits 191a-210b, dates 12/26/2012-06/26/2013
Map 10: Map2013B, year 5, orbits 211a-230b, dates 06/26/2013-12/26/2013
Map 11: Map2014A, year 6, orbits 231a-250b, dates 12/26/2013-06/26/2014
Map 12: Map2014B, year 6, orbits 251a-270b, dates 06/26/2014-12/24/2014
Map 13: Map2015A, year 7, orbits 271a-290b, dates 12/24/2014-06/24/2015
Map 14: Map2015B, year 7, orbits 291a-310b, dates 06/24/2015-12/23/2015
Map 15: Map2016A, year 8, orbits 311a-330b, dates 12/24/2015 . 06/23/2016
Map 16: Map2016B, year 8, orbits 331a-351a, dates 06/24/2016 . 12/26/2016
Map 17: Map2017A, year 9, orbits 351b-371a, dates 12/26/2016 . 06/24/2017
Map 18: Map2017B, year 9, orbits 371b-391a, dates 06/25/2017 . 12/25/2017
Map 19: Map2018A, year 10, orbits 391b-411b, dates 12/25/2017 . 06/28/2018
Map 20: Map2018B, year 10, orbits 412a-431b, dates 06/29/2018 . 12/26/2018
Map 21: Map2019A, year 11, orbits 432a-451b, dates 12/27/2018 . 06/27/2019
Map 22: Map2019B, year 11, orbits 452a-471b, dates 06/28/2019 . 12/26/2019
8: This particular data set, denoted in the original ascii files as
hvset_noSP_antiram_N for N=2009,2019, includes pixel map data from antiram
direction (antiram-directional), no CG, no SP, 1 year cadence. 
Modification History
The Release 16 data extend through Map 22 and contain modications and updates of
Maps 1-2 from Release 2, Maps 1-6 from Release 4, and Maps 1-10 from Release 7,
maps 1-14 from Release 10, maps 15-22 from Release 16. The present CDF data set
was converted from the originally archived data in ascii list format but
otherwise includes no changes in the data. The original data are given in 30
rows for Solar Ecliptic Latitude and 60 columns for Solar Ecliptic East
Longitude. The accompanying documentation described the row latitude data as
starting from the north Ecliptic pole (+90 degrees) and decreasing in value to
the south Ecliptic pole (-90 degrees). During preparation of the data set in CDF
format, SPDF discovered that the correct order was increasing from row 1 for the
South Ecliptic pole to row 30 for the north Ecliptic pole. East longitude is
defined correctly for the column order but we have instead used west longitude
to better represent the outward-looking viewpoint from IBEX to the outer
heliosphere as typically used in IBEX team plots.