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CDAWeb Served Heliophysics Datasets Beginning with 'R'

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-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)

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_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_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)

RS_K0_IPEI: ROCSAT-1(FORMOSAT-1)/IPEI, Key Parameters - Shin-Yi Su (Institution of Space Science, National Central University, Taiwan, R.O.C.)

---

RBSP-A-RBSPICE_LEV-2_ESRHELT doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE High Energy Resolution Electron Rates converted into units of
physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_ESRLEHT doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE Low Energy Resolution Electron Rates converted into units of
physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> Telescope 1: stacked plots by energy [FEDU_stack1]
  -----> Telescope 2 [FEDU_stack2]
  -----> Telescope 3 [FEDU_stack3]
  -----> Telescope 4 [FEDU_stack4]
  -----> Telescope 5 [FEDU_stack5]
  -----> Telescope 6 [FEDU_stack6]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_ISRHELT doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE high energy resolution Ion Species Rates (ISRHELT) converted into
units of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy
resolution and low time resolution.
For more information regarding this data and
the RBSPICE science goals and mission statement see the RBSPICE team web site
at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= ~70 PA) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_TOFXEH doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE TOF x Energy Hydrogen Rates converted into units of physical
intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution and low
time resolution.
For more information regarding this data and the RBSPICE
science goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order [FPDU]
  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_TOFXEION doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE TOF x Energy Ion Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at high energy resolution and low time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_TOFXENONH doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE TOF x E non Hydrogen (Helium and Oxygen) Rates converted into units
of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FHeDU: Helium flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FHeDU]

  The Helium component is measured in the first 9 (per REM) channels of this data
  product. The last 11 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FHeDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in middle 6 channels of this data product. The
  first 11 channels and last 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_TOFXPHHHELT doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE TOF x PH Hydrogen Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at high energy resolution and low time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 20 channels of this data product.
  The frst 11 channels and last channel have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 11 channels of this data product. The
  last 22 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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---

RBSP-A-RBSPICE_LEV-2_TOFXPHHLEHT doi:tbd Copy BibTeX Citation
Proper citations should include the "Accessed on date" in the form .

Description

RBSP RBSPICE TOF x PH Hydrogen Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at low energy resolution and high time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 7 channels of this data product.
  The frst 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 3 channels of this data product. The
  last 7 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_ESRHELT doi:10.48322/7mxy-dn25 Copy BibTeX Citation

Description

rbspa rbspice high energy res low time res electron energy intensities/pressures
sorted by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FEDU: UniDirectional Differential Electron Flux, 20-940 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FEDU]
  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FEDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Quality_ByA_atE]
  Calculated Electron perpendicular partial pressure for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_PerpPressure]
  ---> Calculated Electron parallel partial pressure for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (20Kev-940KeV) and pitch angle for Electrons. Does not include noisy energy channels. [FEDU_Density]
  Pitch Angle and Energy Integrated total intensity of Electrons observed during the spin for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_IntegralFlux]
  Omni Directional Total Electron Flux per spin for energies 20Kev-940KeV [FEDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FEDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FEDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-A-RBSPICE_LEV-3-PAP_ESRLEHT doi:10.48322/ezsz-e525 Copy BibTeX Citation

Description

rbspa rbspice low energy res high time res electron energy intensities/pressures
sorted by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FEDU: UniDirectional Differential Electron Flux, 23-430 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FEDU]
  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FEDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Quality_ByA_atE]
  Calculated Electron perpendicular partial pressure for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_PerpPressure]
  ---> Calculated Electron parallel partial pressure for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (23Kev-430KeV) and pitch angle for Electrons. Does not include noisy energy channels. [FEDU_Density]
  Pitch Angle and Energy Integrated total intensity of Electrons observed during the spin for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_IntegralFlux]
  Omni Directional Total Electron Flux per spin for energies 23Kev-430KeV [FEDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FEDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FEDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_TOFXEH doi:10.48322/t323-cd86 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014
Version 2.0 Skeleton Produced October 1, 2015

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 0.05-0.6 Mev, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_ByA_atE]
  Calculated proton perpendicular partial pressure for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (50Kev-660KeV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 40Kev-660KeV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_TOFXEHE doi:10.48322/knbt-qb86 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe helium intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FHeDU:UniDirectional Differential He Flux, 0.06-0.9 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FHeDU]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FHeDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Quality_ByA_atE]
  Calculated Helium perpendicular partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_PerpPressure]
  Calculated Helium parallel partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (60Kev-590KeV) and pitch angle for Helium. Does not include noisy energy channels. [FHeDU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Helium observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FHeDU_IntegralFlux]
  Omni Directional Total Helium Flux per spin for energies: 60keV-590keV (Counts/(MeV-s-cm^2)) [FHeDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-A-RBSPICE_LEV-3-PAP_TOFXEHE-0 doi:10.48322/z9kh-tp03 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe helium intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FHeDU:UniDirectional Differential He Flux, 0.06-0.6 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FHeDU]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FHeDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Quality_ByA_atE]
  Calculated Helium perpendicular partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_PerpPressure]
  Calculated Helium parallel partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (60Kev-590KeV) and pitch angle for Helium. Does not include noisy energy channels. [FHeDU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Helium observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FHeDU_IntegralFlux]
  Omni Directional Total Helium Flux per spin for energies: 60keV-590keV (Counts/(MeV-s-cm^2)) [FHeDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_TOFXEION doi:10.48322/3wy7-bv28 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe ion intensities/pressures sorted by
pitch angles.

Modification History

Version 1.0 Skeleton Produced August 5, 2015

• Data Variable Descriptions
  FIDU: UniDirectional Differential Ion Flux, 0.04-18.5 Mev, binned by pitch angle in 17 bins (as energy-angle displays) [FIDU]
  ---> Spectrograms by energy at sample pitch angles [FIDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FIDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FIDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. See PREBM standards for definition [FIDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FIDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_Quality_ByA_atE]
  Calculated Ion perpendicular partial pressure for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_PerpPressure]
  ---> Calculated Ion parallel partial pressure for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (48kev-5MeV) and pitch angle for Ions. Does not include noisy energy channels. [FIDU_Density]
  Pitch Angle and Energy Integrated total intensity of Ions observed during the spin for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_IntegralFlux]
  Omni Directional Total Ion Flux per spin for energies 21kev-10MeV [FIDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FIDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FIDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_TOFXEO doi:10.48322/gg52-1338 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 0.14-0.9 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_ByA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 125keV-980keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 125keV-980keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (125kev-980keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 125kev-980keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 125keV-980keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-A-RBSPICE_LEV-3-PAP_TOFXEO-0 doi:10.48322/nw9y-vj72 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 0.14-1.1 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_ByA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_ByA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_ByA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 125keV-1260keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 125keV-1260keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (125keV-1260keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 125keV-1260keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHHHELT doi:10.48322/9j1k-re84 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 7-51 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. See PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_byA_atE]
  Calculated proton perpendicular partial pressure for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (7keV-51keV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 7keV-51keV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHHLEHT doi:10.48322/1393-6m93 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 7-51 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. See PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_byA_atE]
  Calculated proton perpendicular partial pressure for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (7keV-100keV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 7keV-100keV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHOHELT doi:10.48322/wsp2-ds36 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 49-177 keV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. See PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 49-177keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 49-177keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (49-177keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 49-177keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 49-177keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production. The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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---

RBSP-A-RBSPICE_LEV-3-PAP_TOFXPHOLEHT doi:10.48322/q87a-tn74 Copy BibTeX Citation

Description

rbspice low energy res high time res tofxph oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 49-161 keV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 49-161keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 49-161keVkeV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (49-161keVkeV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 49-161keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 49-161keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (49-161keV): Counts/(MeV-cm^2-s) [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (49-161keV): Counts/(MeV-cm^2-s) [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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---

RBSP-A-RBSPICE_LEV-3_ESRHELT doi:10.48322/zcrq-hj26 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res Electron Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FEDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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---

RBSP-A-RBSPICE_LEV-3_ESRLEHT doi:10.48322/n221-vw77 Copy BibTeX Citation

Description

RBSPA RBSPICE Low Energy Res High Time Res Electron Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FEDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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---

RBSP-A-RBSPICE_LEV-3_ISRHELT doi:10.48322/daqq-gk90 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res Ion Energy Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FIDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3_TOFXEH doi:10.48322/e889-c285 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res TOFxE Proton Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order [FPDU]
  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3_TOFXEION doi:10.48322/ee6n-x567 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res TOFxE Ion Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FIDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3_TOFXENONH doi:10.48322/qghx-dt80 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res TOFxE non Proton Intensities with
Pitch Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FHeDU: Helium flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FHeDU]

  The Helium component is measured in the first 9 (per REM) channels of this data
  product. The last 11 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FHeDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in middle 6 channels of this data product. The
  first 11 channels and last 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FHeDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3_TOFXPHHHELT doi:10.48322/nj27-cf05 Copy BibTeX Citation

Description

RBSPA RBSPICE High Energy Res Low Time Res TOFxPH Proton Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 20 channels of this data product.
  The frst 11 channels and last channel have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 11 channels of this data product. The
  last 22 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A-RBSPICE_LEV-3_TOFXPHHLEHT doi:10.48322/jstq-z957 Copy BibTeX Citation

Description

RBSPA RBSPICE Low Energy Res High Time Res TOFxPH Proton Rates converted into
units of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy
resolution and low time resolution which includes RBSPICE Pitch angle and
Magnetic Field derived values. \n For more information regarding this data and
the RBSPICE science goals and mission statement see the RBSPICE team web site
at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 7 channels of this data product.
  The frst 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 3 channels of this data product. The
  last 7 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-A_DENSITY_EMFISIS-L4 doi:10.48322/c4ha-xj50 Copy BibTeX Citation

Description

Density and other parameters inferred by digitizing the trace on the
spectrograms.

• Data Variable Descriptions
  Digitized frequency point, interpreted using value of digi_type [y]
  B-Field magnitude used to infer fce [bmag]
  Electron cyclotron frequency (fce) [fce]
  Electron plasma frequency (fpe) [fpe]
  Ratio of electron plasma oscillation (wpe) to cyclotron gyration (wce) [wpe_over_wce]
  Upper hybrid resonance frequency (fuh) [fuh]
  electron density [density]

  Electron density inferred from spectrogram.
  

  (NO PLOTTING) digi_type: "fuh" means fuh was digitized, or "fpe" means fpe was digitized using cutoffs [digi_type]

  "fuh" or "fpe"
  

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RBSP-A_HFR-SPECTRA-BURST_EMFISIS-L2 doi:10.48322/18b2-kt74 Copy BibTeX Citation

Description

Single Axis AC Electric Field Spectra (Selectable between the U, V and W Axis).
Frequency range: 10 kHz to 486.97kHz    (Band width:480 Hz to 23.231kHz). 82
logarithmically spaced frequency bins. Cadence: 1 spectral matrix per 6 seconds.

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-A_HFR-SPECTRA-MERGED_EMFISIS-L2 doi:10.48322/j4rf-2n06 Copy BibTeX Citation

Description

1

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-A_HFR-SPECTRA_EMFISIS-L2 doi:10.48322/2gay-q957 Copy BibTeX Citation

Description

Single Axis AC Electric Field Spectra (Selectable between the U, V and W Axis).
Frequency range: 10 kHz to 486.97kHz    (Band width:480 Hz to 23.231kHz). 82
logarithmically spaced frequency bins. Cadence: 1 spectral matrix per 6 seconds.

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-A_HFR-WAVEFORM_EMFISIS-L2 doi:10.48322/pg1z-7a92 Copy BibTeX Citation

Description

Single Axis AC Electric Field Waveform (Selectable between the U, V and W Axis).
Units: V/m. Sample Rate: 1 Msample/sec. Sample Size: 4096 samples. Cadence:
variable.

• Data Variable Descriptions
  V/m displayed as spectrogram of values vs time offsets [HFRsamples_spec]
  V/m displayed as very high resolution time-series [HFRsamples_times]
  Attenuator select indicator for U and V axis. 0-Off, 1-On. Switches in a 19 dB attenuator. [HBGain]

  L2 and greater data has the attenuator gains folded into data to provide correct
  science units
  

  ---> Axis channel indicator for the HFR. 0-U axis, 1-V axis, 2-W axis. [HBSelect]
  ---> MET [MET]

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RBSP-A_MAGNETOMETER_1SEC-GEI_EMFISIS-L3 doi:10.48322/esgw-y164 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_1SEC-GEO_EMFISIS-L3 doi:10.48322/2913-5d64 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_1SEC-GSE_EMFISIS-L3 doi:10.48322/s5sk-bm30 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_1SEC-GSM_EMFISIS-L3 doi:10.48322/w6r4-fp76 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector in GSM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_1SEC-SM_EMFISIS-L3 doi:10.48322/4kbj-9183 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in SM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector in SM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_4SEC-GEI_EMFISIS-L3 doi:10.48322/hnyz-nk70 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_4SEC-GEO_EMFISIS-L3 doi:10.48322/zgv3-5m40 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_4SEC-GSE_EMFISIS-L3 doi:10.48322/6f9r-x856 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_4SEC-GSM_EMFISIS-L3 doi:10.48322/zrvq-vt55 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_4SEC-SM_EMFISIS-L3 doi:10.48322/d15r-3a05 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_HIRES-GEI_EMFISIS-L3 doi:10.48322/q8rs-hg23 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GEI [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GEI [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_HIRES-GEO_EMFISIS-L3 doi:10.48322/yhbp-n321 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GEO [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GEO [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_HIRES-GSE_EMFISIS-L3 doi:10.48322/hn0a-s943 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSE [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GSE [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_HIRES-GSM_EMFISIS-L3 doi:10.48322/2tyy-s986 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GSM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_HIRES-SM_EMFISIS-L3 doi:10.48322/h47r-sf90 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in SM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in SM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_MAGNETOMETER_UVW_EMFISIS-L2 doi:10.48322/8ttw-6h90 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in UVW [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-A_WFR-SPECTRAL-MATRIX-DIAGONAL-MERGED_EMFISIS-L2 doi:10.48322/at6y-vy38 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-A_WFR-SPECTRAL-MATRIX-DIAGONAL_EMFISIS-L2 doi:10.48322/3v2f-af86 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  WFR frequencies [WFR_frequencies]

  These are the center of the frequency bands for the power spectra
  

  ---> WFR_bandwidth [WFR_bandwidth]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-A_WFR-SPECTRAL-MATRIX_EMFISIS-L2

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  [NO PLOTS] BuBv amplitude [BuBv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuBw amplitude [BuBw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvBw amplitude [BvBw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  [NO PLOTS] BuEu amplitude [BuEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuEv amplitude [BuEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuEw amplitude [BuEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvEu amplitude [BvEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvEv amplitude [BvEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvEw amplitude [BvEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEu amplitude [BwEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEv amplitude [BwEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEw amplitude [BwEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  [NO PLOTS] EuEv amplitude [EuEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] EuEw amplitude [EuEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] EvEw amplitude [EvEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-A_WFR-WAVEFORM-CONTINUOUS-BURST_EMFISIS-L2 doi:10.48322/czxv-qx38 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  continuous burst waveforms208896 samples @ 35 kS/sec.

• Data Variable Descriptions
  BuSamples (as spectrogram vs Time Offsets) [BuSamples]
  ---> BvSamples [BvSamples]
  ---> BwSamples [BwSamples]
  EuSamples (as spectrogram vs Time Offsets) [EuSamples]
  ---> EvSamples [EvSamples]
  ---> EwSamples [EwSamples]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

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RBSP-A_WFR-WAVEFORM_EMFISIS-L2 doi:10.48322/13vc-c837 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  waveforms16384 samples @ 35 kS/sec...Calibration Notes:.Warning: All L2
Waveform products are calibrated in amplitude at 1kHz only.  There is no phase
calibration applied at this stage...Before using these waveforms to process wave
parameters, please follow the calibration process described below or the results
will be wrong...Level-2 (L2) Waveform data is amplitude-calibrated at 1 kHz. 
But there are amplitude deviations at other frequencies, and there are phase
shifts which are not reflected in the L2 data at all. The phase shift is a
frequency-dependent shift in the phase of the observed wave relative to the
input wave, tantamount to a time delay at that frequency. . .The L2 data can be
adjusted over frequency by applying dimensionless complex factors over frequency
immediately after Fourier transforming the L2 data. The Variables
BCalibrationCoef and ECalibration Coef in the cdf consists of a table for the B
sensors and a table for the E sensors. Each table has 5600 X 2 entries. The 
first column is the real component and the second is the imaginary component of
the calibration, extending from 2.13623 to 11962.89 Hz, in steps of 2.13623 Hz 
(Variable: CalFrequencies contains the associated frequencies of the calibration
coeficients). Above the highest frequency the WFR filters roll off; no
calibration measurements exist, but one could apply the last value to any
frequencies above that.. .The table is constructed assuming 16384 data points
are to be FFT'ed. If fewer than that are to be transformed, then the table can
be decimated to accommodate a shorter data set. The procedure is;  FFT the L2
data at the desired resolution and then perform a complex multiplication of the
FFT'ed dataset  and the E or B adjustment table.. .If comparing results of the
frequency-adjusted L2 data with the onboard survey spectra, note that the L2
data has units of volts/meter and nanoTesla for E and B respectively, whereas
the onboard survey spectra have units of RMS volts/meter and RMS nanoTesla.. 

• Data Variable Descriptions
  BuSamples (as spectrogram vs Time Offsets) [BuSamples]
  ---> BvSamples [BvSamples]
  ---> BwSamples [BwSamples]
  EuSamples (as spectrogram vs Time Offsets) [EuSamples]
  ---> EvSamples [EvSamples]
  ---> EwSamples [EwSamples]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

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RBSP-A_WNA-SURVEY-SHEATH-CORRECTED-E_EMFISIS-L4

Description

Wave Normal Analysis products, based on L1 spectral matrix survey E and B data,
and produced via PRASSADCO (Santolik, et al., Radio Sci., 38(1), 1010, 2003). A
correction for antenna sheath effects has been applied to the electric field
data, before being input to PRASSADCO. The correction is density-dependent, so
fill values are inserted for E-dependent data where a density estimate is not
available.
 Be aware that the spin-plane E antennas began deployment at 2012-09-13T19:44,
and were not fully deployed until 2012-09-22T19:48. The spin-axis deployment
began on 2012-09-24T17:59 and did not fully complete until 2012-12-07T04:41.
Noise levels in the E data are increased by incomplete antenna deployment.
 There was a significant upgrade to the onboard calibration tables, for both E
and B in Feb 2013. Prior to this, the highest survey frequency bin (11.24 kHz)
used a flawed cal value that resulted in both amplitude and phase errors. The
effect is stronger for the B data. New, corrected, tables took effect at
2013-02-12T04:30:00.
 In Mar 2013, there was a ~2-day interval where a software issue resulted in the
wrong calibration tables being used for both E and B data. These data should be
used with extreme caution. The interval is 2013-03-21T06:53:00 to
2013-03-23T05:46:00.

• Data Variable Descriptions
  Power Spectral Density of B!bparallel!n [b3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Sum of the Three Magnetic Power Spectral Densities [bsum]
  Sum of Two Perpendicular Magnetic Power Spectral Densities [bsumperp]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward. Perpendicular components are along axis1 (outward)
  and axis2 (eastward).
  

  Coherence Between B!bperp1!n and B!bperp2!n [cohb1_2]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Coherence Between B!bperp1!n and B!bpar!n [cohb1_3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Coherence Between B!bperp2!n and B!bpar!n [cohb2_3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Power Spectral Density of E!bparallel!n [ez]

  Coordinate system is field-aligned, with Z along B0, X outward from the Earth,
  and Y eastward.
  

  Power Spectral Density of E!bparallel!n Using Faraday Law [ezf]

  Does not use measured spin-axis E data when calculating E components in
  field-aligned system. Spin-axis E is synthesized from the two spin-plane E and
  all three B components, using Faraday law and plane-wave assumption (Sec. 3.3,
  Santolik, et al., Radio Sci., 38(1), 1010, 2003). Coordinate system is
  field-aligned, with Z along B0, X outward from the Earth, and Y eastward.
  

  Sum of the Three Electric Power Spectral Densities [esum]
  Sum of Two Perpendicular Electric Power Spectral Densities [esumperp]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward. Perpendicular components are along axis1 (outward)
  and along axis2 (eastward).
  

  Sum of Two Perpendicular Electric Power Spectral Densities Using Faraday Law [esumperpf]

  Does not use measured spin-axis E data when calculating E components in
  field-aligned system. Spin-axis E is synthesized from the two spin-plane E and
  all three B components, using Faraday law and plane-wave assumption (Sec. 3.3,
  Santolik, et al., Radio Sci., 38(1), 1010, 2003). Coordinate system is
  field-aligned, with axis3 along B0, axis1 outward from the Earth, and axis2
  eastward. Perpendicular components are along axis1 (outward) and along axis2
  (eastward).
  

  Degree of Polarization of The Magnetic Field From Eigenvalues [eigen]

  Eigenvalues are determined using the SVD method (Santolik, et al., Radio Sci.,
  38(1), 1010, 2003)
  

  Ellipticity of the Magnetic Field Polarization [ellsvd]

  Determined using the SVD method, from eq. 13 of Santolik, et al., Radio Sci.,
  38(1), 1010, 2003
  

  Degree of Magnetic Field Polarization in the Polarization Plane [polsvd]

  Determined using the SVD method, from eq. A6 in the appendix of Santolik, et
  al., J. Geophys. Res., 107(A12), 1444, 2002.
  

  Planarity of the Magnetic Field Polarization [plansvd]

  Determined using the SVD method, from eq. 12 of Santolik, et al., Radio Sci.,
  38(1), 1010, 2003.
  

  Electromagnetic Planarity [plansvde]

  Electromagnetic planarity calculated from the 6x6 spectral matrix using eq. 24
  of Santolik, et al., Radio Sci., 38(1), 1010, 2003.
  

  Polar Angle of the Wave Vector [thsvd]

  Wave Normal Angles are determined using the SVD method (Santolik, et al., Radio
  Sci., 38(1), 1010, 2003). Angle is measured from axis3, but all angles are 0 <=
  theta <= 90, due to ambiguity in the SVN method. Coordinate system is
  field-aligned, with axis3 along B0.
  

  Azimuthal Angle of the Wave Vector [phsvd]

  Wave Normal Angles are determined using the SVD method (Santolik, et al., Radio
  Sci., 38(1), 1010, 2003). Angle is measured counterclockwise from axis1.
  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Spectral Density of the Poynting Flux [poy1_2_3]

  Poynting flux is directly computed from the E and B spectral data, in the
  field-aligned system, with axis3 along B0, axis1 outward from the Earth, and
  axis2 eastward.
  

  Polar Angle of the Poynting Vector [thpoy1_2_3]

  Angle is measured from axis3. Poynting flux is directly computed from the E and
  B spectral data, in the field-aligned system, with axis3 along B0, axis1 outward
  from the Earth, and axis2 eastward.
  

  Azimuthal Angle of the Poynting Vector [phpoy1_2_3]

  Angle is measured counterclockwise from axis1. Poynting flux is directly
  computed from the E and B spectral data, in the field-aligned system, with axis3
  along B0, axis1 outward from the Earth, and axis2 eastward.
  

  Spectral Density of the Poynting Flux Using Faraday Law [poyf1_2_3]

  Poynting flux is directly computed from the E and B spectral data, in the
  field-aligned system, with axis3 along B0, axis1 outward from the Earth, and
  axis2 eastward. Does not use measured spin-axis E data when calculating E
  components in field-aligned system. Spin-axis E is synthesized from the two
  spin-plane E and all three B components, using Faraday law and plane-wave
  assumption (Sec. 3.3, Santolik, et al., Radio Sci., 38(1), 1010, 2003).
  

  Polar Angle of the Poynting Vector Using Faraday Law [thpoyf1_2_3]

  Angle is measured from axis3. Poynting flux is directly computed from the E and
  B spectral data, in the field-aligned system, with axis3 along B0, axis1 outward
  from the Earth, and axis2 eastward. Does not use measured spin-axis E data when
  calculating E components in field-aligned system. Spin-axis E is synthesized
  from the two spin-plane E and all three B components, using Faraday law and
  plane-wave assumption (Sec. 3.3, Santolik, et al., Radio Sci., 38(1), 1010,
  2003).
  

  Azimuthal Angle of the Poynting Vector Using Faraday Law [phpoyf1_2_3]

  Angle is measured counterclockwise from axis1. Poynting flux is directly
  computed from the E and B spectral data, in the field-aligned system, with axis3
  along B0, axis1 outward from the Earth, and axis2 eastward. Does not use
  measured spin-axis E data when calculating E components in field-aligned system.
  Spin-axis E is synthesized from the two spin-plane E and all three B components,
  using Faraday law and plane-wave assumption (Sec. 3.3, Santolik, et al., Radio
  Sci., 38(1), 1010, 2003).
  

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RBSP-B-RBSPICE_LEV-2_ESRHELT doi:10.48322/2zcv-0b61 Copy BibTeX Citation

Description

RBSP RBSPICE High Energy Resolution Electron Rates converted into units of
physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_ESRLEHT doi:10.48322/btrq-0a49 Copy BibTeX Citation

Description

RBSP RBSPICE Low Energy Resolution Electron Rates converted into units of
physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> Telescope 1: stacked plots by energy [FEDU_stack1]
  -----> Telescope 2 [FEDU_stack2]
  -----> Telescope 3 [FEDU_stack3]
  -----> Telescope 4 [FEDU_stack4]
  -----> Telescope 5 [FEDU_stack5]
  -----> Telescope 6 [FEDU_stack6]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_ISRHELT doi:10.48322/gd0d-6e49 Copy BibTeX Citation

Description

RBSP RBSPICE high energy resolution Ion Species Rates (ISRHELT) converted into
units of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy
resolution and low time resolution.
For more information regarding this data and
the RBSPICE science goals and mission statement see the RBSPICE team web site
at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= ~70 PA) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_TOFXEH doi:10.48322/49dp-jw39 Copy BibTeX Citation

Description

RBSP RBSPICE TOF x Energy Hydrogen Rates converted into units of physical
intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution and low
time resolution.
For more information regarding this data and the RBSPICE
science goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order [FPDU]
  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_TOFXEION doi:10.48322/jt55-m188 Copy BibTeX Citation

Description

RBSP RBSPICE TOF x Energy Ion Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at high energy resolution and low time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_TOFXENONH doi:10.48322/v4tx-ej55 Copy BibTeX Citation

Description

RBSP RBSPICE TOF x E non Hydrogen (Helium and Oxygen) Rates converted into units
of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy resolution
and low time resolution.
For more information regarding this data and the
RBSPICE science goals and mission statement see the RBSPICE team web site at:
http:// rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FHeDU: Helium flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FHeDU]

  The Helium component is measured in the first 9 (per REM) channels of this data
  product. The last 11 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FHeDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in middle 6 channels of this data product. The
  first 11 channels and last 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_TOFXPHHHELT doi:10.48322/4qe2-5145 Copy BibTeX Citation

Description

RBSP RBSPICE TOF x PH Hydrogen Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at high energy resolution and low time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 20 channels of this data product.
  The frst 11 channels and last channel have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 11 channels of this data product. The
  last 22 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-2_TOFXPHHLEHT doi:10.48322/2jc4-tb70 Copy BibTeX Citation

Description

RBSP RBSPICE TOF x PH Hydrogen Rates converted into units of physical intensity
(counts/(s*sr*cm^2*MeV) measured at low energy resolution and high time
resolution.
For more information regarding this data and the RBSPICE science
goals and mission statement see the RBSPICE team web site at: http:// 
rbspice.ftecs.com.

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 7 channels of this data product.
  The frst 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 3 channels of this data product. The
  last 7 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L]
  ---> Position of the spacecraft in SM coordinates [Position_SM]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame and taken from the definitive SPICE SPK kernels that are available at the time. [L_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_ESRHELT doi:10.48322/yean-0a44 Copy BibTeX Citation

Description

rbspb rbspice high energy res low time res electron energy intensities/pressures
sorted by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FEDU: UniDirectional Differential Electron Flux, 20-940 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FEDU]
  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FEDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Quality_byA_atE]
  Calculated Electron perpendicular partial pressure for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_PerpPressure]
  ---> Calculated Electron parallel partial pressure for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (20Kev-940KeV) and pitch angle for Electrons. Does not include noisy energy channels. [FEDU_Density]
  Pitch Angle and Energy Integrated total intensity of Electrons observed during the spin for energies 20Kev-940KeV. Does not include noisy energy channels. [FEDU_IntegralFlux]
  Omni Directional Total Electron Flux per spin for energies 20Kev-940KeV [FEDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FEDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FEDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_ESRLEHT doi:10.48322/yq1a-4q76 Copy BibTeX Citation

Description

rbspb rbspice low energy res high time res electron energy intensities/pressures
sorted by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FEDU: UniDirectional Differential Electron Flux, 23-430 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FEDU]
  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FEDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FEDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_Quality_byA_atE]
  Calculated Electron perpendicular partial pressure for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_PerpPressure]
  ---> Calculated Electron parallel partial pressure for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (23Kev-430KeV) and pitch angle for Electrons. Does not include noisy energy channels. [FEDU_Density]
  Pitch Angle and Energy Integrated total intensity of Electrons observed during the spin for energies 23Kev-430KeV. Does not include noisy energy channels. [FEDU_IntegralFlux]
  Omni Directional Total Electron Flux per spin for energies 23Kev-430KeV [FEDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FEDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FEDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_TOFXEH doi:10.48322/6n22-6807 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014
Version 2.0 Skeleton Produced October 1, 2015

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 0.05-0.6 Mev, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_byA_atE]
  Calculated proton perpendicular partial pressure for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (50Kev-660KeV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 50Kev-660KeV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 40Kev-660KeV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE doi:10.48322/0nfn-gt73 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe helium intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FHeDU:UniDirectional Differential He Flux, 0.06-0.9 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FHeDU]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FHeDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Quality_byA_atE]
  Calculated Helium perpendicular partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_PerpPressure]
  Calculated Helium parallel partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (60Kev-590KeV) and pitch angle for Helium. Does not include noisy energy channels. [FHeDU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Helium observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FHeDU_IntegralFlux]
  Omni Directional Total Helium Flux per spin for energies: 60keV-590keV (Counts/(MeV-s-cm^2)) [FHeDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE-0 doi:10.48322/dkyf-gz14 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe helium intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FHeDU:UniDirectional Differential He Flux, 0.06-0.6 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FHeDU]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FHeDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FHeDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FHeDU_Quality_byA_atE]
  Calculated Helium perpendicular partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_PerpPressure]
  Calculated Helium parallel partial pressure for energies: 60Kev-590KeV. Does not include noisy energy channels. [FHeDU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (60Kev-590KeV) and pitch angle for Helium. Does not include noisy energy channels. [FHeDU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Helium observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FHeDU_IntegralFlux]
  Omni Directional Total Helium Flux per spin for energies: 60keV-590keV (Counts/(MeV-s-cm^2)) [FHeDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FHeDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_TOFXEION doi:10.48322/ke3e-5s15 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxeion ion intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced August 5, 2015

• Data Variable Descriptions
  FIDU: UniDirectional Differential Ion Flux, 0.04-18.5 Mev, binned by pitch angle in 17 bins (as energy-angle displays) [FIDU]
  ---> Spectrograms by energy at sample pitch angles [FIDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FIDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FIDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FIDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FIDU_Quality_byA_atE]
  Calculated Ion perpendicular partial pressure for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_PerpPressure]
  ---> Calculated Ion parallel partial pressure for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (48kev-5MeV) and pitch angle for Ions. Does not include noisy energy channels. [FIDU_Density]
  Pitch Angle and Energy Integrated total intensity of Ions observed during the spin for energies 48kev-5MeV. Does not include noisy energy channels. [FIDU_IntegralFlux]
  Omni Directional Total Ion Flux per spin for energies 21kev-10MeV [FIDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FIDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FIDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO doi:10.48322/7bnw-z839 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 0.06-0.9 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 125keV-980keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 125keV-980keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (125keV-980keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 125keV-980keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 125keV-980keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO-0 doi:10.48322/2c4e-dk29 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxe oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 0.14-1.1 MeV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 125keV-1260keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 125keV-1260keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (125keV-1260keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 60kev-590keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 125keV-1260keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHHELT doi:10.48322/7dg0-7h47 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 7-51 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_byA_atE]
  Calculated proton perpendicular partial pressure for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (7keV-51keV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 7keV-51keV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 7keV-51keV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHLEHT doi:10.48322/njhg-7j22 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph proton intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FPDU: UniDirectional Differential Proton Flux, 7-51 keV, binned by pitch angle in 17 bins (as energy-angle displays) [FPDU]
  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FPDU_Error]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FPDU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_Quality_byA_atE]
  Calculated proton perpendicular partial pressure for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_PerpPressure]
  ---> Calculated proton parallel partial pressure for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_ParaPressure]
  ---> Number Density calculated by integrating the distribution function over energy (7keV-100keV) and pitch angle for protons. Does not include noisy energy channels. [FPDU_Density]
  Pitch Angle and Energy Integrated total intensity of protons observed during the spin for energies 7keV-100keV. Does not include noisy energy channels. [FPDU_IntegralFlux]
  Omni Directional Total Proton Flux per spin for energies 7keV-100keV [FPDU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel [FPDU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel [FPDU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOHELT doi:10.48322/hrv9-ec37 Copy BibTeX Citation

Description

rbspice high energy res low time res tofxph oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 49-177 keV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 49-177keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 49-177keV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (49-177keV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 49-177keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 49-177keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (60keV-590keV): Counts/(MeV-cm^2-s) [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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---

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOLEHT doi:10.48322/bwm7-5m36 Copy BibTeX Citation

Description

rbspice low energy res high time res tofxph oxygen intensities/pressures sorted
by pitch angles.

Modification History

Version 1.0 Skeleton Produced July 29, 2014

• Data Variable Descriptions
  FODU:UniDirectional Differential Oxygen Flux, 49-161 keV, one record per spin binned by pitch angle in 17 bins (as energy-angle displays) [FODU]
  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_byA_atE]
  The Poisson statistical counting percentage error of the measurement for each energy channel and bin calculated as 1/sqrt(Counts)*100. [FODU_Error]
  ---> Spectrograms by energy at sample pitch angles [FODU_Error_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Error_byA_atE]
  Quality flag for the measurement for each pitch angle bin/timestep. .see PREBM standards for definition [FODU_Quality]
  ---> Spectrograms by energy at sample pitch angles [FODU_Quality_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FODU_Quality_byA_atE]
  Calculated Oxygen perpendicular partial pressure for energies: 49-161keV. Does not include noisy energy channels. [FODU_PerpPressure]
  Calculated Oxygen parallel partial pressure for energies: 49-161keVkeV. Does not include noisy energy channels. [FODU_ParaPressure]
  The Number Density (#/cm^3) calculated by integrating the distribution function over energy (49-161keVkeV) and pitch angle for Oxygen. Does not include noisy energy channels. [FODU_Density]
  Pitch Angle Integrated and Energy Integrated total intensity of Oxygen observed during the spin for energies: 49-161keV. Does not include noisy energy channels. [FODU_IntegralFlux]
  Omni Directional Total Oxygen Flux per spin for energies: 49-161keV (Counts/(MeV-s-cm^2)) [FODU_OmniFlux]
  ---> Observed minimum intensity in the spin for each energy channel measured (49-161keV): Counts/(MeV-cm^2-s) [FODU_MinimFlux]
  ---> Observed maximum intensity in the spin for each energy channel measured (49-161keV): Counts/(MeV-cm^2-s) [FODU_MaximFlux]
  Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the spacecraft in SM coordinates [Position_SM]

  Position of the spacecraft at MidET in the SM (Solar Magnetospheric) reference
  frame using the definition SPICE kernels available at production..The position
  varies with time and contains the position for the X, Y, and Z axis of the SC in
  Earth Radii.
  

  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B-RBSPICE_LEV-3_ESRHELT doi:10.48322/vn20-5g44 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res Electron Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Level 1.3 version produced December 20, 2012
L

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum; T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FEDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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RBSP-B-RBSPICE_LEV-3_ESRLEHT doi:10.48322/nxsw-2k50 Copy BibTeX Citation

Description

RBSPB RBSPICE Low Energy Res High Time Res Electron Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FEDU: Electron flux spectrograms in energy, by telescope in sector order (T0= ~110 PA, T3= ~all PAs, T5= FEDU background) [FEDU]
  ---> The percentage error of the measurement. [FEDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FEDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FEDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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---

RBSP-B-RBSPICE_LEV-3_ISRHELT doi:10.48322/1t5a-gm85 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res Ion Energy Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FIDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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---

RBSP-B-RBSPICE_LEV-3_TOFXEH doi:10.48322/6crc-aj02 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res TOFxE Proton Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order [FPDU]
  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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RBSP-B-RBSPICE_LEV-3_TOFXEION doi:10.48322/1qnv-8c11 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res TOFxE Ion Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FIDU: Ion flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FIDU]
  ---> The percentage error of the measurement. [FIDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FIDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FIDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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RBSP-B-RBSPICE_LEV-3_TOFXENONH doi:10.48322/w7nq-kz93 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res TOFxE non Proton Intensities with
Pitch Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FHeDU: Helium flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FHeDU]

  The Helium component is measured in the first 9 (per REM) channels of this data
  product. The last 11 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FHeDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FHeDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in middle 6 channels of this data product. The
  first 11 channels and last 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FHeDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
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RBSP-B-RBSPICE_LEV-3_TOFXPHHHELT doi:10.48322/6wj8-zz20 Copy BibTeX Citation

Description

RBSPB RBSPICE High Energy Res Low Time Res TOFxPH Proton Intensities with Pitch
Angles converted into units of physical intensity (counts/(s*sr*cm^2*MeV)
measured at high energy resolution and low time resolution which includes
RBSPICE Pitch angle and Magnetic Field derived values. \n For more information
regarding this data and the RBSPICE science goals and mission statement see the
RBSPICE team web site at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 20 channels of this data product.
  The frst 11 channels and last channel have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 11 channels of this data product. The
  last 22 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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---

RBSP-B-RBSPICE_LEV-3_TOFXPHHLEHT doi:10.48322/9f4c-2b63 Copy BibTeX Citation

Description

RBSPB RBSPICE Low Energy Res High Time Res TOFxPH Proton Rates converted into
units of physical intensity (counts/(s*sr*cm^2*MeV) measured at high energy
resolution and low time resolution which includes RBSPICE Pitch angle and
Magnetic Field derived values. \n For more information regarding this data and
the RBSPICE science goals and mission statement see the RBSPICE team web site
at: http:// rbspice.ftecs.com. 

Modification History

Skeleton Produced June 6, 2012
Version 1.3 produced December 20, 2012
L

• Data Variable Descriptions
  FPDU: Proton flux spectrograms in energy, by telescope in sector order (spin accums plotted at end of accum) [FPDU]

  The Proton component is measured in the last 7 channels of this data product.
  The frst 3 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FPDU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FPDU_Quality]
  ---> The current sector number where each spin is divided into 36 sectors. [Sector]
  ---> Duration of the accumulation. [Duration]
  ---> The current spin number of the spacecraft [Spin]
  FODU: Oxygen flux spectrograms in energy, by telescope in sector order (multi-spin accums plotted at end of accum) [FODU]

  The Oxygen component is measured in first 3 channels of this data product. The
  last 7 channels have values of a default value.
  

  ---> The percentage error of the measurement. [FODU_Error]
  ---> Quality flag for the measurement for each telescope/channel/timestep. .see PREBM standards for definition [FODU_Quality]
  Position of the spacecraft in SM coordinates [Position_SM]
  ---> Position of the SC in the GEO Reference Frame. [Position]
  ---> Position of the SC in the GSM Reference Frame. [Position_GSM]
  ---> The position quality flag, 0=good, 1=bad. [Position_Quality]
  Orbit Number at the time of the measurement [OrbitNumber]
  ---> Dipole L value calculated using the SM Reference Frame [L]
  ---> McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq]
  ---> Roeder's L* value (derived from ECT MagEphem data) for the average pitch angle. [L_Star]
  ---> Integral invariant for the average pitch angle derived from ECT MagEphem data. [I]
  ---> The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K]
  ---> Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT]
  The pitch angle based upon the look direction of each telescope, alpha=cos-1(B*(-look)) [FPDU_Alpha]

  Identical to Alpha
  

  ---> A flag describing the Quality of the Pitch Angle as calculated, 0=good, 1=bad. [Alpha_Quality]
  The particle velocity unit vector for each telescope look direction (i.e. the negative of the telescope look direction unit vector). (No CDAWeb Plotting) [ParticleDir_SM]
  Roeder's L* value (derived from ECT MagEphem data) for each of the telescopes based upon the telescope pitch angle. [L_StarArr]
  ---> The Integral invariant for the pitch angle of each telescope derived from ECT MagEphem data. [IArr]
  ---> Second Invariant ( I*sqrt(Bm) ) for the pitch angle of each telescope derived from ECT MagEphem data. [KArr]
  [Labels on plots] Position of the spacecraft in SM coordinates [Position_SM_TT]
  ---> [Labels on plots] Position of the SC in the GEO Reference Frame. [Position_TT]
  ---> [Labels on plots] Position of the SC in the GSM Reference Frame. [Position_GSM_TT]
  [Labels on plots] Orbit Number at the time of the measurement [OrbitNumber_TT]
  ---> [Labels on plots] Dipole L value calculated using the SM Reference Frame [L_TT]
  ---> [Labels on plots] McElqain L value calculated at the Equator (derived from ECT MagEphem data). [L_Eq_TT]
  ---> [Labels on plots] Roeder's L* value(derived from ECT MagEphem data) for the average pitch angle. [L_Star_TT]
  ---> [Labels on plots] Integral invariant for the average pitch angle derived from ECT MagEphem data. [I_TT]
  ---> [Labels on plots] The Second Invariant ( I*sqrt(Bm) ) for the average pitch angle derived from ECT MagEphem data. [K_TT]
  ---> [Labels on plots] Magnetic Local Time of S/C in Centerted Dipole Coordinates derived from ECT MagEphem data. [MLT_TT]

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RBSP-B_DENSITY_EMFISIS-L4 doi:10.48322/c6s1-wg66 Copy BibTeX Citation

Description

Density and other parameters inferred by digitizing the trace on the
spectrograms.

• Data Variable Descriptions
  Digitized frequency point, interpreted using value of digi_type [y]
  B-Field magnitude used to infer fce [bmag]
  Electron cyclotron frequency (fce) [fce]
  Electron plasma frequency (fpe) [fpe]
  Ratio of electron plasma oscillation (wpe) to cyclotron gyration (wce) [wpe_over_wce]
  Upper hybrid resonance frequency (fuh) [fuh]
  electron density [density]

  Electron density inferred from spectrogram.
  

  (NO PLOTTING) digi_type: "fuh" means fuh was digitized, or "fpe" means fpe was digitized using cutoffs [digi_type]

  "fuh" or "fpe"
  

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RBSP-B_HFR-SPECTRA-BURST_EMFISIS-L2 doi:10.48322/prbv-3b62 Copy BibTeX Citation

Description

Single Axis AC Electric Field Spectra (Selectable between the U, V and W Axis).
Frequency range: 10 kHz to 486.97kHz    (Band width:480 Hz to 23.231kHz). 82
logarithmically spaced frequency bins. Cadence: 1 spectral matrix per 6 seconds.

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-B_HFR-SPECTRA-MERGED_EMFISIS-L2 doi:10.48322/g03f-pz86 Copy BibTeX Citation

Description

1

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-B_HFR-SPECTRA_EMFISIS-L2 doi:10.48322/zpmq-qm18 Copy BibTeX Citation

Description

Single Axis AC Electric Field Spectra (Selectable between the U, V and W Axis).
Frequency range: 10 kHz to 486.97kHz    (Band width:480 Hz to 23.231kHz). 82
logarithmically spaced frequency bins. Cadence: 1 spectral matrix per 6 seconds.

• Data Variable Descriptions
  HFR Spectra Data [HFR_Spectra]
  ---> HFR center band frequencies [HFR_frequencies]
  ---> HFR bin size - Number of bins summed on board [HFR_bins]
  ---> HFR Gain Select (0 - Standard Gain, 1 - Attenuator On) [HBGain]
  ---> HFR receiver Antenna Select (0 - U axis,1 - V axis,2 - W axis {spin axis}) [HBSelect]
  ---> MET [MET]

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RBSP-B_HFR-WAVEFORM_EMFISIS-L2 doi:10.48322/dz64-x875 Copy BibTeX Citation

Description

Single Axis AC Electric Field Waveform (Selectable between the U, V and W Axis).
Units: V/m. Sample Rate: 1 Msample/sec. Sample Size: 4096 samples. Cadence:
variable.

• Data Variable Descriptions
  V/m displayed as spectrogram of values vs time offsets [HFRsamples_spec]
  V/m displayed as very high resolution time-series [HFRsamples_times]
  Attenuator select indicator for U and V axis. 0-Off, 1-On. Switches in a 19 dB attenuator. [HBGain]

  L2 and greater data has the attenuator gains folded into data to provide correct
  science units
  

  ---> Axis channel indicator for the HFR. 0-U axis, 1-V axis, 2-W axis. [HBSelect]
  ---> MET [MET]

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RBSP-B_MAGNETOMETER_1SEC-GEI_EMFISIS-L3 doi:10.48322/8zvn-5753 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_1SEC-GEO_EMFISIS-L3 doi:10.48322/9fmv-3p17 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_1SEC-GSE_EMFISIS-L3 doi:10.48322/xhkc-6v40 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_1SEC-GSM_EMFISIS-L3 doi:10.48322/x429-5310 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector in GSM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_1SEC-SM_EMFISIS-L3 doi:10.48322/fg6n-yr78 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in SM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector in SM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_4SEC-GEI_EMFISIS-L3 doi:10.48322/7gy4-qd32 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_4SEC-GEO_EMFISIS-L3 doi:10.48322/5zd2-dk98 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_4SEC-GSE_EMFISIS-L3 doi:10.48322/e698-nb28 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_4SEC-GSM_EMFISIS-L3 doi:10.48322/kh8k-hc54 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_4SEC-SM_EMFISIS-L3 doi:10.48322/knn2-mp16 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  B-rms (total standard deviation in B over averaging interval) [rms]
  S/C position vector [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_HIRES-GEI_EMFISIS-L3 doi:10.48322/b30v-s029 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GEI [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GEI [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_HIRES-GEO_EMFISIS-L3 doi:10.48322/y09z-a990 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GEO [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GEO [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_HIRES-GSE_EMFISIS-L3 doi:10.48322/mdts-0y61 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSE [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GSE [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_HIRES-GSM_EMFISIS-L3 doi:10.48322/4dx1-s250 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in GSM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in GSM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_HIRES-SM_EMFISIS-L3 doi:10.48322/k10e-1w74 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in SM [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  S/C position vector in SM [coordinates]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_MAGNETOMETER_UVW_EMFISIS-L2 doi:10.48322/66f8-6c92 Copy BibTeX Citation

Description

3 axis Fluxgate Magnetometer data.  Sampled onboard at 64 vectors per second.  3
range states available,  Range 0 (+/- 256 nT),  Range 1 (+/- 4096 nT), Range 3
(+/- 65536 nT).

• Data Variable Descriptions
  Magnetometer vector in UVW [Mag]
  Average magnitude (average of |B| values in the interval) [Magnitude]
  Latitude (angle delta) of the field vector (where (0,0) is the positive Bx direction) [delta]
  Longitude (angle lambda) of the field vector (where (0,0) is the positive Bx direction) [lambda]
  range_flag [range_flag]
  ---> partition [partition]
  ---> MET [MET]
  ---> calState_flag [calState]
  ---> magInvalid_flag [magInvalid]
  ---> magFill_flag [magFill]

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RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL-MERGED_EMFISIS-L2 doi:10.48322/0ch5-t113 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL_EMFISIS-L2 doi:10.48322/dafd-6p95 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  WFR frequencies [WFR_frequencies]

  These are the center of the frequency bands for the power spectra
  

  ---> WFR_bandwidth [WFR_bandwidth]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-B_WFR-SPECTRAL-MATRIX_EMFISIS-L2 doi:10.48322/abqk-a365 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  cross spectral matrix,  6 diagonal components and 15 off-diagonal
components.Frequency range: 10 kHz to 487kHz..82 Frequency Bins.Cadence: 1
spectra per 6 seconds (survey).

• Data Variable Descriptions
  BuBu amplitude [BuBu]

  Autocorrelation of the U axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BvBv amplitude [BvBv]

  Autocorrelation of the V axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  ---> BwBw amplitude [BwBw]

  Autocorrelation of the W axis of the Search Coil.  Base science coordinate
  system (UVW)
  

  EuEu amplitude [EuEu]

  Autocorrelation of the U axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EvEv amplitude [EvEv]

  Autocorrelation of the V axis of the Electric Field.  Base science coordinate
  system (UVW)
  

  ---> EwEw amplitude [EwEw]

  Autocorrelation of the W axis of the Electric Field.  Base science coordinate
  system (UVW). Warning: the aft boom is shadowed by the fixed booms on the
  spacecraft, thus producing periodic spikes in the data due to photoelectron
  modulation.
  

  [NO PLOTS] BuBv amplitude [BuBv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuBw amplitude [BuBw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvBw amplitude [BvBw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  [NO PLOTS] BuEu amplitude [BuEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuEv amplitude [BuEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BuEw amplitude [BuEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOT] BvEu amplitude [BvEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvEv amplitude [BvEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BvEw amplitude [BvEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEu amplitude [BwEu]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEv amplitude [BwEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] BwEw amplitude [BwEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  [NO PLOTS] EuEv amplitude [EuEv]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] EuEw amplitude [EuEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  ---> [NO PLOTS] EvEw amplitude [EvEw]

  Complex number (real + imaginary) .Depend 1 0 -  Real, 1 - Imagninary
  

  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> MET [MET]

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RBSP-B_WFR-WAVEFORM-CONTINUOUS-BURST_EMFISIS-L2 doi:10.48322/gm07-2739 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  continuous burst waveforms208896 samples @ 35 kS/sec.

• Data Variable Descriptions
  BuSamples (as spectrogram vs Time Offsets) [BuSamples]
  ---> BvSamples [BvSamples]
  ---> BwSamples [BwSamples]
  EuSamples (as spectrogram vs Time Offsets) [EuSamples]
  ---> EvSamples [EvSamples]
  ---> EwSamples [EwSamples]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

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RBSP-B_WFR-WAVEFORM_EMFISIS-L2 doi:10.48322/mf9b-6r41 Copy BibTeX Citation

Description

Three Axis Electric Field (EU, EV, EW) and Three Axis Magnetic field (BU, BV,
BW)  waveforms16384 samples @ 35 kS/sec...Calibration Notes:.Warning: All L2
Waveform products are calibrated in amplitude at 1kHz only.  There is no phase
calibration applied at this stage...Before using these waveforms to process wave
parameters, please follow the calibration process described below or the results
will be wrong...Level-2 (L2) Waveform data is amplitude-calibrated at 1 kHz. 
But there are amplitude deviations at other frequencies, and there are phase
shifts which are not reflected in the L2 data at all. The phase shift is a
frequency-dependent shift in the phase of the observed wave relative to the
input wave, tantamount to a time delay at that frequency. . .The L2 data can be
adjusted over frequency by applying dimensionless complex factors over frequency
immediately after Fourier transforming the L2 data. The Variables
BCalibrationCoef and ECalibration Coef in the cdf consists of a table for the B
sensors and a table for the E sensors. Each table has 5600 X 2 entries. The 
first column is the real component and the second is the imaginary component of
the calibration, extending from 2.13623 to 11962.89 Hz, in steps of 2.13623 Hz 
(Variable: CalFrequencies contains the associated frequencies of the calibration
coeficients). Above the highest frequency the WFR filters roll off; no
calibration measurements exist, but one could apply the last value to any
frequencies above that.. .The table is constructed assuming 16384 data points
are to be FFT'ed. If fewer than that are to be transformed, then the table can
be decimated to accommodate a shorter data set. The procedure is;  FFT the L2
data at the desired resolution and then perform a complex multiplication of the
FFT'ed dataset  and the E or B adjustment table.. .If comparing results of the
frequency-adjusted L2 data with the onboard survey spectra, note that the L2
data has units of volts/meter and nanoTesla for E and B respectively, whereas
the onboard survey spectra have units of RMS volts/meter and RMS nanoTesla.. 

• Data Variable Descriptions
  BuSamples (as spectrogram vs Time Offsets) [BuSamples]
  ---> BvSamples [BvSamples]
  ---> BwSamples [BwSamples]
  EuSamples (as spectrogram vs Time Offsets) [EuSamples]
  ---> EvSamples [EvSamples]
  ---> EwSamples [EwSamples]
  Attenuator select indicator for W axis (0=off) [LWEzGainW]

  Attenuator select indicator for W axis.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.   L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

  ---> Attenuator select indicator for U/V axes (0=off) [LWExEyGainUV]

  Attenuator select indicator for U and V axis.  0 - Off, 1 - On.   Switches in a
  19 dB attenuator.  L2 and greater data has the attenuator gains folded into data
  to provide correct science units.
  

  ---> Attenuator select indicator for MSC (0=off) [SCMGain]

  Attenuator select indicator for MSC.  0 - Off, 1 - On.   Switches in a 19 dB
  attenuator.  L2 and greater data has the attenuator gains folded into data to
  provide correct science units. 
  

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RBSP-B_WNA-SURVEY-SHEATH-CORRECTED-E_EMFISIS-L4

Description

Wave Normal Analysis products, based on L1 spectral matrix survey E and B data,
and produced via PRASSADCO (Santolik, et al., Radio Sci., 38(1), 1010, 2003). A
correction for antenna sheath effects has been applied to the electric field
data, before being input to PRASSADCO. The correction is density-dependent, so
fill values are inserted for E-dependent data where a density estimate is not
available.
 Be aware that the spin-plane E antennas began deployment at 2012-09-13T23:06,
and were not fully deployed until 2012-09-22T22:32. The spin-axis deployment
began on 2012-09-24T20:33 and did not fully complete until 2012-12-07T17:25.
Noise levels in the E data are increased by incomplete antenna deployment.
 There was a significant upgrade to the onboard calibration tables, for both E
and B in Feb 2013. Prior to this, the highest survey frequency bin (11.24 kHz)
used a flawed cal value that resulted in both amplitude and phase errors. The
effect is stronger for the B data. New, corrected, tables took effect at
2013-02-13T01:48:00.
 In Mar 2013, there was a ~2-day interval where a software issue resulted in the
wrong calibration tables being used for both E and B data. These data should be
used with extreme caution. The interval is 2013-03-21T09:35:00 to
2013-03-23T02:07:00.

• Data Variable Descriptions
  Power Spectral Density of B!bparallel!n [b3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Sum of the Three Magnetic Power Spectral Densities [bsum]
  Sum of Two Perpendicular Magnetic Power Spectral Densities [bsumperp]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward. Perpendicular components are along axis1 (outward)
  and axis2 (eastward).
  

  Coherence Between B!bperp1!n and B!bperp2!n [cohb1_2]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Coherence Between B!bperp1!n and B!bpar!n [cohb1_3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Coherence Between B!bperp2!n and B!bpar!n [cohb2_3]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Power Spectral Density of E!bparallel!n [ez]

  Coordinate system is field-aligned, with Z along B0, X outward from the Earth,
  and Y eastward.
  

  Power Spectral Density of E!bparallel!n Using Faraday Law [ezf]

  Does not use measured spin-axis E data when calculating E components in
  field-aligned system. Spin-axis E is synthesized from the two spin-plane E and
  all three B components, using Faraday law and plane-wave assumption (Sec. 3.3,
  Santolik, et al., Radio Sci., 38(1), 1010, 2003). Coordinate system is
  field-aligned, with Z along B0, X outward from the Earth, and Y eastward.
  

  Sum of the Three Electric Power Spectral Densities [esum]
  Sum of Two Perpendicular Electric Power Spectral Densities [esumperp]

  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward. Perpendicular components are along axis1 (outward)
  and along axis2 (eastward).
  

  Sum of Two Perpendicular Electric Power Spectral Densities Using Faraday Law [esumperpf]

  Does not use measured spin-axis E data when calculating E components in
  field-aligned system. Spin-axis E is synthesized from the two spin-plane E and
  all three B components, using Faraday law and plane-wave assumption (Sec. 3.3,
  Santolik, et al., Radio Sci., 38(1), 1010, 2003). Coordinate system is
  field-aligned, with axis3 along B0, axis1 outward from the Earth, and axis2
  eastward. Perpendicular components are along axis1 (outward) and along axis2
  (eastward).
  

  Degree of Polarization of The Magnetic Field From Eigenvalues [eigen]

  Eigenvalues are determined using the SVD method (Santolik, et al., Radio Sci.,
  38(1), 1010, 2003)
  

  Ellipticity of the Magnetic Field Polarization [ellsvd]

  Determined using the SVD method, from eq. 13 of Santolik, et al., Radio Sci.,
  38(1), 1010, 2003
  

  Degree of Magnetic Field Polarization in the Polarization Plane [polsvd]

  Determined using the SVD method, from eq. A6 in the appendix of Santolik, et
  al., J. Geophys. Res., 107(A12), 1444, 2002.
  

  Planarity of the Magnetic Field Polarization [plansvd]

  Determined using the SVD method, from eq. 12 of Santolik, et al., Radio Sci.,
  38(1), 1010, 2003.
  

  Electromagnetic Planarity [plansvde]

  Electromagnetic planarity calculated from the 6x6 spectral matrix using eq. 24
  of Santolik, et al., Radio Sci., 38(1), 1010, 2003.
  

  Polar Angle of the Wave Vector [thsvd]

  Wave Normal Angles are determined using the SVD method (Santolik, et al., Radio
  Sci., 38(1), 1010, 2003). Angle is measured from axis3, but all angles are 0 <=
  theta <= 90, due to ambiguity in the SVN method. Coordinate system is
  field-aligned, with axis3 along B0.
  

  Azimuthal Angle of the Wave Vector [phsvd]

  Wave Normal Angles are determined using the SVD method (Santolik, et al., Radio
  Sci., 38(1), 1010, 2003). Angle is measured counterclockwise from axis1.
  Coordinate system is field-aligned, with axis3 along B0, axis1 outward from the
  Earth, and axis2 eastward.
  

  Spectral Density of the Poynting Flux [poy1_2_3]

  Poynting flux is directly computed from the E and B spectral data, in the
  field-aligned system, with axis3 along B0, axis1 outward from the Earth, and
  axis2 eastward.
  

  Polar Angle of the Poynting Vector [thpoy1_2_3]

  Angle is measured from axis3. Poynting flux is directly computed from the E and
  B spectral data, in the field-aligned system, with axis3 along B0, axis1 outward
  from the Earth, and axis2 eastward.
  

  Azimuthal Angle of the Poynting Vector [phpoy1_2_3]

  Angle is measured counterclockwise from axis1. Poynting flux is directly
  computed from the E and B spectral data, in the field-aligned system, with axis3
  along B0, axis1 outward from the Earth, and axis2 eastward.
  

  Spectral Density of the Poynting Flux Using Faraday Law [poyf1_2_3]

  Poynting flux is directly computed from the E and B spectral data, in the
  field-aligned system, with axis3 along B0, axis1 outward from the Earth, and
  axis2 eastward. Does not use measured spin-axis E data when calculating E
  components in field-aligned system. Spin-axis E is synthesized from the two
  spin-plane E and all three B components, using Faraday law and plane-wave
  assumption (Sec. 3.3, Santolik, et al., Radio Sci., 38(1), 1010, 2003).
  

  Polar Angle of the Poynting Vector Using Faraday Law [thpoyf1_2_3]

  Angle is measured from axis3. Poynting flux is directly computed from the E and
  B spectral data, in the field-aligned system, with axis3 along B0, axis1 outward
  from the Earth, and axis2 eastward. Does not use measured spin-axis E data when
  calculating E components in field-aligned system. Spin-axis E is synthesized
  from the two spin-plane E and all three B components, using Faraday law and
  plane-wave assumption (Sec. 3.3, Santolik, et al., Radio Sci., 38(1), 1010,
  2003).
  

  Azimuthal Angle of the Poynting Vector Using Faraday Law [phpoyf1_2_3]

  Angle is measured counterclockwise from axis1. Poynting flux is directly
  computed from the E and B spectral data, in the field-aligned system, with axis3
  along B0, axis1 outward from the Earth, and axis2 eastward. Does not use
  measured spin-axis E data when calculating E components in field-aligned system.
  Spin-axis E is synthesized from the two spin-plane E and all three B components,
  using Faraday law and plane-wave assumption (Sec. 3.3, Santolik, et al., Radio
  Sci., 38(1), 1010, 2003).
  

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RBSPA_EFW-L2_E-HIRES-UVW doi:10.48322/qtvb-dd97 Copy BibTeX Citation

Description

High Resolution DC Electric Field in UVW Coordinates.

Modification History

v01:  initial version.

• Data Variable Descriptions
  Efield (UVW) [e_hires_uvw]

  DC electric field in the UVW coordinate system at 16 or 32 samples/sec
  

  Efield raw (UVW) [e_hires_uvw_raw]

  DC electric field in the UVW coordinate system at 16 or 32 samples/sec, without
  spinning-frame offset removal
  

  Spin Axis Vector in GSE [L_vector]

  Angular momentum/spin axis direction of spacecraft spin, namely, the sunward
  pointing direction of spacecraft spin axis.
  

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RBSPA_EFW-L2_E-SPINFIT-MGSE doi:10.48322/rhve-mz23 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spacraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

Modification History

v01:  initial version.

• Data Variable Descriptions
  Spinfit E-field in MGSE (autoscale, VxB subtracted, i.e. near GSE) [efield_spinfit_mgse]

  Spin-fit electric field esimate in the MGSE coordinate system and GSE frame (VxB
  subtracted) derived from the EFW e12 (V1-V2) data product.
  

  ---> Spinfit E-field in MGSE (fixedscale, VxB subtracted, i.e. near GSE) [efield_spinfit_mgse_fixedscale]

  Spin-fit electric field esimate in the MGSE coordinate system and GSE frame (VxB
  subtracted) derived from the EFW e12 (V1-V2) data product.
  

  VxB E-field in MGSE coordinates. [VxB_mgse]

  Electric field due to VxB, where V is spacecraft velocity and B is the measured
  ambient magnetic field.
  

  ---> Corotation Efield (MGSE) [efield_coro_mgse]

  Corotation electric field
  

  EFW quality array (global estimate of EFW data quality, plus 13 underlying observatory and instrument-level data quality factors) [e_spinfit_mgse_efw_qual]
  Bias current [bias_current]

  Bias current (nA) applied to the antenna probes 
  

  L_vector (spin axis GSE) [spinaxis_gse]

  Pointing direction (GSE) defining the spacecraft angular velocity (spinaxis w
  component)
  

  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [flags_all]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_DUNNO (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

  ---> MLT [mlt]

  Magnetic local time
  

  ---> MLat [mlat]

  magnetic latitude
  

  ---> L [lshell]

  lshell from simple dipole model
  

  ---> Lstar [Lstar]

  Lstar
  

  S/C position in GSE [pos_gse]

  Spacecraft position in GSE coordinates
  

  ---> S/C velocity in GSE [vel_gse]

  Spacecraft velocity in km/s in the GSE coordinate system
  

  ---> Orbit number [orbit_num]

  orbit number
  

  Angles b/t the Ey and Ez MGSE spinplane directions and the background magnetic field. [angle_Ey_Ez_Bo]

  Angle b/t the Ey(Ez) MGSE spinplane directions and the background magnetic
  field. Used to test when the E*B=0 assumption is appropriate
  

  diagEx1 [diagEx1]

  Diagnostic quantity 1 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagEx2 [diagEx2]

  Diagnostic quantity 2 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagBratio [diagBratio]

  Diagnostic variable with By/Bx and Bz/Bx for the E*B=0 calculation
  

  flags_charging_bias_eclipse [flags_charging_bias_eclipse]

  charging, bias, eclipse flags, extreme charging
  

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RBSPA_EFW-L2_ESVY_DESPUN doi:10.48322/t40m-em97 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spacraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

Modification History

v01:  initial version.

• Data Variable Descriptions
  Despun E-field in MGSE (32 S/s, VxB subtracted, near GSE) [efield_mgse]

  electric field in the MGSE coordinate system
  

  ---> EFW quality array (global estimate of EFW data quality, plus 13 underlying observatory and instrument-level data quality factors) [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  
  
  See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual.
  
  If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2).
  
  If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_DUNNO (typ. -1).
  
  A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual.
  
  The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

  orbit_num [orbit_num]

  orbit number
  

  MLT [mlt]

  Magnetic local time from ECT's predicted Ephemeris
  

  ---> Mlat [mlat]

  Magnetic latitude from ECT's predicted Ephemeris
  

  ---> Lshell (simple dipole, from ECT predicted Ephermis) [lshell]

  Simple dipole Lshell from ECT's predicted Ephemeris
  

  ---> GSE position [pos_gse]

  GSE position in km from SPICE
  

  ---> GSE velocity [vel_gse]

  GSE velocity in km/s from SPICE
  

  L_vector [spinaxis_gse]

  Pointing direction (GSE) defining the spacecraft angular velocity (spinaxis w
  component)
  

  bias_current [bias_current]

  Bias current (nA) applied to the antenna probes 
  

  diagEx1 [diagEx1]

  Diagnostic quantity 1 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagEx2 [diagEx2]

  Diagnostic quantity 2 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagBratio [diagBratio]

  Diagnostic variable with By/Bx and Bz/Bx for the E*B=0 calculation
  

  flags_charging_bias_eclipse [flags_charging_bias_eclipse]

  charging, bias, eclipse, extreme charging flags
  

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RBSPA_EFW-L2_FBK doi:10.48322/6a7j-p736 Copy BibTeX Citation

Description

Up to two sources are returned. The possible sources are:
E12DC, E34DC,E56DC,
E12AC,E34AC,E56AC,
SCMU,SCMV,SCMW
(V1DC+V2DC+V3DC+V4DC)/4

• Data Variable Descriptions
  Filterbank 13 (<=2013 Mar16) E12DC peak values [fbk13_e12dc_pk]
  ---> Low frequency values overlaid [fbk13_e12dc_pk_lowoverlay]
  Filterbank 13 E34DC peak values [fbk13_e34dc_pk]
  Filterbank 13 (<=2013 Mar16) SCMw peak values [fbk13_scmw_pk]
  ---> Low frequency values overlaid [fbk13_scmw_pk_lowoverlay]
  Filterbank 13 (<=2013 Mar16) E12DC average values [fbk13_e12dc_av]
  ---> Low frequency values overlaid [fbk13_e12dc_av_lowoverlay]
  Filterbank 13 E34DC average values [fbk13_e34dc_av]
  Filterbank 13 (<=2013 Mar16) SCMw average values [fbk13_scmw_av]
  ---> Low frequency values overlaid [fbk13_scmw_av_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) E12DC peak values [fbk7_e12dc_pk]
  ---> Low frequency values overlaid [fbk7_e12dc_pk_lowoeverlay]
  Filterbank 7 (Early 2012) SCMu peak values [fbk7_scmu_pk]
  Filterbank 7 (>=2013 Mar 17) SCMw peak values [fbk7_scmw_pk]
  ---> Low frequency values overlaid [fbk7_scmw_pk_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) E12DC average values [fbk7_e12dc_av]
  Filterbank 7 (Early 2012) SCMu average values [fbk7_scmu_av]
  ---> Low frequency values overlaid [fbk7_e12dc_av_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) SCMw average values [fbk7_scmw_av]
  ---> Low frequency values overlaid [fbk7_scmw_av_lowoverlay]
  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_UNK (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

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RBSPA_EFW-L2_SPEC doi:10.48322/78pf-4k59 Copy BibTeX Citation

Description

Six spectral products are returned. The possible sources
are:.E12dc,E34dc,E56dc.E12ac,E34ac,E56ac.Edcpar,Edcprp.Eacpar,Eacprp.V1ac,V2ac,V
3ac,V4ac,V5ac,V6ac.SCMU,SCMV,SCMW.SCMpar,SCMprp,.(V1ac+V2ac+V3ac+V4ac)/4,.Edcprp
2, Eacprp2, SCMprp2.

Caveats

See THEMIS website for caveats

• Data Variable Descriptions
  E12 AC [spec64_e12ac]

  64 bin spectrogram for E12AC
  

  spec64_e12dc [spec64_e12dc]

  64 bin spectrogram for E12DC
  

  ---> E56 AC [spec64_e56ac]

  64 bin spectrogram for E56AC
  

  spec64_e34dc [spec64_e34dc]

  64 bin spectrogram for E34DC
  

  [64 FREQUENCIES] V1 AC [spec64_v1ac]

  64 bin spectrogram for V1AC
  

  spec64_e34ac [spec64_e34ac]

  64 bin spectrogram for E34AC
  

  ---> V2 AC [spec64_v2ac]

  64 bin spectrogram for V2AC
  

  spec64_e56dc [spec64_e56dc]

  64 bin spectrogram for E56DC
  

  [64 FREQUENCIES] SCM u [spec64_scmu]

  64 bin spectrogram for SCMu
  

  ---> SCM v [spec64_scmv]

  64 bin spectrogram for SCMv
  

  spec64_epar_dc [spec64_epardc]

  64 bin spectrogram for Eparallel DC
  

  ---> SCM w [spec64_scmw]

  64 bin spectrogram for SCMw
  

  spec64_eperp1dc [spec64_eperp1dc]

  64 bin spectrogram for Eperp1 DC
  

  spec64_eparac [spec64_eparac]

  64 bin spectrogram for Eparallel AC
  

  spec64_eperp1ac [spec64_eperp1ac]

  64 bin spectrogram for Eperp1 AC
  

  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_UNK (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

  spec64_v3ac [spec64_v3ac]

  64 bin spectrogram for V3AC
  

  spec64_v4ac [spec64_v4ac]

  64 bin spectrogram for V4AC
  

  spec64_v5ac [spec64_v5ac]

  64 bin spectrogram for V5AC
  

  spec64_v6ac [spec64_v6ac]

  64 bin spectrogram for V6AC
  

  spec64_scmpar [spec64_scmpar]

  64 bin spectrogram for SCMpar
  

  spec64_scmperp1 [spec64_scmperp1]

  64 bin spectrogram for SCMperp1
  

  spec64_v1234_avg [spec64_v1234_avg]

  64 bin spectrogram for (v1+v2+v3+v4)/4
  

  spec64_eperp2dc [spec64_eperp2dc]

  64 bin spectrogram for Eperp2 DC
  

  spec64_eperp2ac [spec64_eperp2ac]

  64 bin spectrogram for Eperp2 AC
  

  spec64_scmperp2 [spec64_scmperp2]

  64 bin spectrogram for SCMperp2
  

  spec36_e12dc [spec36_e12dc]
  spec36_e12ac [spec36_e12ac]
  spec36_e34dc [spec36_e34dc]
  spec36_e34ac [spec36_e34ac]
  spec36_e56dc [spec36_e56dc]
  spec36_e56ac [spec36_e56ac]
  spec36_epardc [spec36_epardc]
  spec36_eperp1dc [spec36_eperp1dc]
  spec36_eparac [spec36_eparac]
  spec36_eperp1ac [spec36_eperp1ac]
  spec36_v1ac [spec36_v1ac]
  spec36_v2ac [spec36_v2ac]
  spec36_v3ac [spec36_v3ac]
  spec36_v4ac [spec36_v4ac]
  spec36_v5ac [spec36_v5ac]
  spec36_v6ac [spec36_v6ac]
  spec36_scmu [spec36_scmu]
  spec36_scmv [spec36_scmv]
  spec36_scmw [spec36_scmw]
  spec36_scmpar [spec36_scmpar]
  spec36_scmperp1 [spec36_scmperp1]
  spec36_v1234_avg [spec36_v1234_avg]
  spec36_eperp2dc [spec36_eperp2dc]
  spec36_eperp2ac [spec36_eperp2ac]
  spec36_scmperp2 [spec36_scmperp2]
  spec112_e12dc [spec112_e12dc]
  spec112_e12ac [spec112_e12ac]
  spec112_e34dc [spec112_e34dc]
  spec112_e34ac [spec112_e34ac]
  spec112_e56dc [spec112_e56dc]
  spec112_e56ac [spec112_e56ac]
  spec112_epardc [spec112_epardc]
  spec112_eperp1dc [spec112_eperp1dc]
  spec112_eparac [spec112_eparac]
  spec112_eperp1ac [spec112_eperp1ac]
  spec112_v1ac [spec112_v1ac]
  spec112_v2ac [spec112_v2ac]
  spec112_v3ac [spec112_v3ac]
  spec112_v4ac [spec112_v4ac]
  spec112_v5ac [spec112_v5ac]
  spec112_v6ac [spec112_v6ac]
  spec112_scmu [spec112_scmu]
  spec112_scmv [spec112_scmv]
  spec112_scmw [spec112_scmw]
  spec112_scmpar [spec112_scmpar]
  spec112_scmperp1 [spec112_scmperp1]
  spec112_v1234_avg [spec112_v1234_avg]
  spec112_eperp2dc [spec112_eperp2dc]
  spec112_eperp2ac [spec112_eperp2ac]
  spec112_scmperp2 [spec112_scmperp2]

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RBSPA_EFW-L2_VSVY-HIRES doi:10.48322/7mwt-de58 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spacraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

• Data Variable Descriptions
  potential [vsvy]

  Single-ended antenna potentials
  

  vsvy_vavg [vsvy_vavg]

  Average of opposing antenna potentials. Units of volts
  

  orbit_num [orbit_num]

  orbit number
  

  Velocity (GSE) [vel_gse]

  Spacecraft velocity in km/s in the GSE coordinate system
  

  Position (GSE) [pos_gse]

  Spacecraft position in GSE coordinates
  

  mlt [mlt]

  Magnetic local time
  

  mlat [mlat]

  magnetic latitude
  

  lshell [lshell]

  lshell from simple dipole model
  

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RBSPA_EFW_BURST-WAVEFORM-UVW-L1 doi:10.48322/jcd5-kf50 Copy BibTeX Citation

Description

No TEXT global attribute value.

• Data Variable Descriptions

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RBSPA_L2-1MIN_PSBR-RPS doi:10.48322/h4my-4k78 Copy BibTeX Citation

Description

The RPS instrument is a solid state detector telescope combined with a Cherenkov
radiator. It measures protons with energies from about 60 MeV to about 2 GeV.
For more information, see .http://rbsp.aerospace.org/. For a complete description 
of the instrument, see Mazur et al., 2012, The Relativistic Proton Spectrometer
(RPS) for the Van Allen Probes Mission (formerly known as Radiation Belt Storm
Probes, RBSP), Space Science Reviews. DOI 10.1007/s11214-012-9926-9, 
http://www.springerlink.com/content/p84680786570g7qp/. The instrument PI, Dr.
Joe Mazur, can be reached at Joseph.E.Mazur@aero.org.

Modification History

TBD

• Data Variable Descriptions
  Seconds of livetime in minute [Seconds]
  MET at mid-point of minute [MET_SEC]
  Mission day of level 0 files for this data point [Mission_Day]
  Spacecraft Position (GEO) [Position]
  Position quality flag: 0 - definitive, 1 - predicted [Position_Quality]
  Orbit number [Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [Orbit_Status]
  Decimal hours since perigee [Orbit_Epoch]
  Half-angle of Earth as seen from Spacecraft [EarthConeAngle]
  Measured magnetic field vector in GEO [B_Meas]
  Source of Measured field - 0 indicates MAG L0 file, 1 indicates MAG L1 file, etc. If 255, then the OPQ77 model field is used for computing Alpha and Beta [B_Meas_Flag]
  RPS spin axis vector in GEO vector norm is spin rate [SPIN_OMEGA]
  Counts in data channels based on EVENT_ENERGY_MIN2SSD [DATA_CHANNEL_COUNTS]
  Unidirectional, differential flux vs energy (Isotropic assumption) [FPDI]

  FPDI = Flux Protons Differential Isotropic
  

  RMS error in ln(FPDI) including Poisson and Crosscal Errors [FPDI_RMSE]

  FPDI = Flux Protons Differential Isotropic
  

  Quality flag for FPDI fluxes: 0 - highest quality, 1 - problem with time resolution, 2 - contamination, 3 - saturation, 4 - other problem, 5 - possible electron background, 10 -not yet quality checked [FPDI_Quality]

  FPDI = Flux Protons Differential Isotropic
  

  Mission-Accumulated Dose in Dosimeter 1 (front) [DOSE1]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Dose rate in Dosimeter 1 (front) [DOSE1_RATE]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Mission-Accumulated Dose in Dosimeter 2 (side) [DOSE2]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  Dose rate in Dosimeter 2 (side) [DOSE2_RATE]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  McIlwain L of locally mirroring particle in OPQ [L]

  OPQ
  

  Roederer L of particle with 90 degree pitch angle in OPQ [L_star]

  OPQ
  

  Third (drift) invariant of particle with 90 degree pitch angle in OPQ [Phi]

  OPQ
  

  Equatorial pitch angle of particle with 90 degree pitch angle in OPQ [Alpha_Eq]

  OPQ
  

  OPQ model magnetic field vector in GEO [B_Calc]

  OPQ
  

  OPQ model magnetic field strength at local minimum along local field line [B_Eq]

  OPQ
  

  Magnetic local time (OPQ) [MLT]

  OPQ
  

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RBSPA_L2_PSBR-RPS doi:10.48322/a587-0r70 Copy BibTeX Citation

Description

The RPS instrument is a solid state detector telescope combined with a Cherenkov
radiator. It measures protons with energies from about 60 MeV to about 2 GeV.
For more information, see .http://rbsp.aerospace.org/. For a complete description 
of the instrument, see Mazur et al., 2012, The Relativistic Proton Spectrometer
(RPS) for the Van Allen Probes Mission (formerly known as Radiation Belt Storm
Probes, RBSP), Space Science Reviews. DOI 10.1007/s11214-012-9926-9, 
http://www.springerlink.com/content/p84680786570g7qp/. The instrument PI, Dr.
Joe Mazur, can be reached at Joseph.E.Mazur@aero.org.

Modification History

TBD

• Data Variable Descriptions
  MET at mid-point of sector [MET_SEC]
  Mission day of level 0 files for this data point [Mission_Day]
  Spacecraft Position (GEO) [Position]
  Position quality flag: 0 - definitive, 1 - predicted [Position_Quality]
  Attitude quality flag: 0 - definitive, 1 - quick-look, 2 - predicted [Attitude_Quality]
  Orbit number [Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [Orbit_Status]
  Decimal hours since perigee [Orbit_Epoch]
  Angle of incidence of particle coming from center of Earth (relative to normal incidence) [EarthRadialAngle]
  Half-angle of Earth as seen from Spacecraft [EarthConeAngle]
  Measured magnetic field vector in GEO [B_Meas]
  Source of Measured field - 0 indicates MAG L0 file, 1 indicates MAG L1 file, etc. If 255, then the OPQ77 model field is used for computing Alpha and Beta [B_Meas_Flag]
  RPS bore sight vector in GEO (parallel to incoming normally incident particle) [BORE_SIGHT]

  Unit vector
  

  RPS spin axis vector in GEO vector norm is spin rate [SPIN_OMEGA]
  Counts in data channels based on EVENT_ENERGY_MIN2SSD [DATA_CHANNEL_COUNTS]
  Unidirectional, differential flux vs energy [FPDU]

  FPDU = Flux Protons Differential Unidirectional
  

  RMS error in ln(FPDU) including Poisson and FPDU_Crosscalib_RMSE [FPDU_RMSE]

  FPDU = Flux Protons Differential Unidirectional
  

  Quality flag for FPDU fluxes: 0 - highest quality, 1 - problem with time resolution (less than 5% live time in sector), 2 - contamination, 3 - saturation, 4 - other problem, 5 - possible electron background, 10 -not yet quality checked [FPDU_Quality]

  FPDU = Flux Protons Differential Unidirectional
  

  Mission-Accumulated Dose in Dosimeter 1 (front) [DOSE1]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Dose rate in Dosimeter 1 (front) [DOSE1_RATE]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Mission-Accumulated Dose in Dosimeter 2 (side) [DOSE2]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  Dose rate in Dosimeter 2 (side) [DOSE2_RATE]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  McIlwain L of locally mirroring particle in OPQ [L90]

  OPQ
  

  Pitch angle of incoming particle along RPS boresight axis [Alpha]
  Gyrophase angle of incoming particle along RPS boresight axis (zero when heading away from Earth) [Beta]
  Spin phase angle of RPS boresight. Phase of 0 occurs at minimum pitch angle. Phase of 90 occurs when Alpha is 90 and increasing [SPIN_PHASE]

  Spin phase 0 occurs at minimum pitch angle. Spin phase90 occures at Alpha=90,
  increasing, and this is the fiducial for defining the spin phase. Spin phase 180
  occurs at maximum pitch angle. Spin phase 270 occurs at Alpha=90, decreasing.
  

  Magnetic field strength at mirror point for incoming particle along RPS boresight axis [B_Mirror]
  Equatorial pitch angle (OPQ) of incoming particle along RPS boresight axis [Alpha_Eq]

  OPQ
  

  McIlwain L of normally incident particle in OPQ [L]

  OPQ
  

  Roederer L of normally incident particle in OPQ [L_star]

  OPQ
  

  Third (drift) invariant of normally incident particle in OPQ [Phi]

  OPQ
  

  McIlwain integral invariant of normally incident particle in OPQ [I]

  OPQ
  

  Kaufmann K, modified second invariant, of normally incident particle in OPQ [K]

  OPQ
  

  OPQ model magnetic field vector in GEO [B_Calc]

  OPQ
  

  OPQ model magnetic field strength at local minimum along local field line [B_Eq]

  OPQ
  

  Magnetic local time (OPQ) [MLT]

  OPQ
  

  Minimum geodetic altitude on drift orbit of normally incident particle in OPQ [h_min]

  OPQ
  

  Equatorial pitch angle (T89Q) of incoming particle along RPS boresight axis [Alpha_Eq_T89Q]
  McIlwain L of normally incident particle in T89Q [L_T89Q]
  Roederer L of normally incident particle in T89Q [L_star_T89Q]
  Third (drift) invariant of normally incident particle in T89Q [Phi_T89Q]
  McIlwain integral invariant of normally incident particle in T89Q [I_T89Q]
  Kaufmann K, modified second invariant, of normally incident particle in T89Q [K_T89Q]
  T89Q model magnetic field vector in GEO [B_Calc_T89Q]
  T89Q model magnetic field strength at local minimum along local field line [B_Eq_T89Q]
  Magnetic local time (T89Q) [MLT_T89Q]
  Minimum geodetic altitude on drift orbit of normally incident particle in T89Q [h_min_T89Q]
  Equatorial pitch angle (T89D) of incoming particle along RPS boresight axis [Alpha_Eq_T89D]
  McIlwain L of normally incident particle in T89D [L_T89D]
  Roederer L of normally incident particle in T89D [L_star_T89D]
  Third (drift) invariant of normally incident particle in T89D [Phi_T89D]
  McIlwain integral invariant of normally incident particle in T89D [I_T89D]
  Kaufmann K, modified second invariant, of normally incident particle in T89D [K_T89D]
  T89D model magnetic field vector in GEO [B_Calc_T89D]
  T89D model magnetic field strength at local minimum along local field line [B_Eq_T89D]
  Magnetic local time (T89D) [MLT_T89D]
  Minimum geodetic altitude on drift orbit of normally incident particle in T89D [h_min_T89D]
  Equatorial pitch angle (TS04D) of incoming particle along RPS boresight axis [Alpha_Eq_TS04D]
  McIlwain L of normally incident particle in TS04D [L_TS04D]
  Roederer L of normally incident particle in TS04D [L_star_TS04D]
  Third (drift) invariant of normally incident particle in TS04D [Phi_TS04D]
  McIlwain integral invariant of normally incident particle in TS04D [I_TS04D]
  Kaufmann K, modified second invariant, of normally incident particle in TS04D [K_TS04D]
  TS04D model magnetic field vector in GEO [B_Calc_TS04D]
  TS04D model magnetic field strength at local minimum along local field line [B_Eq_TS04D]
  Magnetic local time (TS04D) [MLT_TS04D]
  Minimum geodetic altitude on drift orbit of normally incident particle in TS04D [h_min_TS04D]
  MET of event, combination of Packet's MET_SEC and EVENT_SUBTIME_CODE [EVENT_MET]

  Not unique
  

  Mission day of level 0 files for this data point [EVENT_Mission_Day]
  Spacecraft Position (GEO) [EVENT_Position]
  Orbit number [EVENT_Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [EVENT_Orbit_Status]
  Decimal hours since perigee [EVENT_Orbit_Epoch]
  McIlwain L of locally mirroring particle in OPQ [EVENT_L90]

  OPQ
  

  McIlwain L of incoming particle along RPS boresight axis [EVENT_L]

  OPQ
  

  Magnetic local time (OPQ) [EVENT_MLT]

  OPQ
  

  Pitch angle of incoming particle along RPS boresight axis [EVENT_Alpha]
  Gyrophase angle of incoming particle along RPS boresight axis (zero when heading away from Earth) [EVENT_Beta]
  Magnetic field strength at mirror point for incoming particle along RPS boresight axis [EVENT_B_Mirror]
  Equatorial pitch angle (OPQ) of incoming particle along RPS boresight axis [EVENT_Alpha_Eq]

  OPQ
  

  D1-D9 detector pulse heights [EVENT_PULSEHEIGHTS]
  D1-D8 Energy Deposit [EVENT_ENERGY_DEPOSIT]
  Coulombs deposited in MCP behind Cherenkov Radiator [EVENT_D9_COULOMBS]
  Photons collected in Cherenkov Radiator [EVENT_CHE_PHOTONS]
  0 - forward, 1 - backward [EVENT_DIRECTION]
  Estimated event energy (uses EVENT_ENERGY_MIN2SSD) [EVENT_ENERGY]
  Estimated event energy using the average of minimum 2 SSD deposits algorithm [EVENT_ENERGY_MIN2SSD]
  Estimated event energy using SSD average algorithm [EVENT_ENERGY_SSDA]
  Estimated event energy using the Cherenkov light only [EVENT_ENERGY_CHE]
  Standard error of ln(EVENT_ENERGY) [EVENT_SIGMA_E]
  ID number of data channel to which the particle is assigned [EVENT_CHANNEL_ID]
  Event classification (-1:INVALID, 0:UNKNOWN, 1:PEN, 2:CHE, 3:ALPHA mode, 127:FILL) [EVENT_TYPE]

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RBSPA_REL03_ECT-MAGEIS-L2 doi:10.48322/dhj8-f337 Copy BibTeX Citation

Description

MagEIS consists of 4 energetic particle sensors per RBSP spacecraft: low unit,
medium35 unit, medium75 unit and the high unit.  The low and 2 medium units are
magnetic spectrometers that measure electrons across roughly the 20 keV - 1 MeV
energy range. The high unit contains a magnetic spectrometer that measures
electrons from roughly the 700 keV to 4 MeV range. The high unit also has a
proton telescope that measures protons from roughly 50 keV to 20 MeV, Helium
ions from roughly 300 keV - 1.5 MeV and Oxygen ions from roughly 1-5 MeV. 
MagEIS is one of three instrument packages on the ECT instrument suite (HOPE and
REPT are the others).

• Data Variable Descriptions
  FESA: Spin-Averaged Differential Electron Flux ~20-4000 keV [FESA]

  Spin-Averaged Differential Electron Flux (FESA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 25 magEIS energy channels. The
  energy channel centroids are specified in FESA_Energy. The channel widths are
  specified in FESA_Energy_Widths. 
  

  ---> FESA as stacked time series [FESA_T]
  ---> % Error in FESA [FESA_ERROR]

  Estimate of the percent error in the uncorrected electron flux.  The percent
  error is defined as a relative error: d(Flux)/Flux, where Flux is the
  uncorrected electron flux.
  

  ---> FESA Quality flag [FESA_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  FESA_CORR: Background-corrected Spin-Averaged Differential Electron Flux ~20-4000 keV [FESA_CORR]

  Spin-Averaged Differential Electron Flux (FESA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 25 magEIS energy channels. The
  energy channel centroids are specified in FESA_Energy. The channel widths are
  specified in FESA_Energy_Widths. 
  

  ---> FESA corrected as stacked time series [FESA_CORR_T]
  ---> % error in FESA corrected [FESA_CORR_ERROR]

  Estimate of the percent error in the background corrected electron flux.  The
  percent error is defined as a relative error: d(Flux)/Flux, where Flux is the
  background corrected electron flux.
  

  FPSA: Spin-Averaged Differential Proton Flux ~50-1500 keV [FPSA]

  Spin-Averaged Differential Proton Flux (FPSA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 31 magEIS energy channels. If
  less than 31 channels are used the remaining channel dimensions are set to fill
  values. The energy channel centroids are specified in FPSA_Energy. The channel
  widths are specified in FPSA_Energy_Widths. 
  

  ---> FPSA as stacked time series [FPSA_T]
  ---> % error in FPSA [FPSA_ERROR]

  Estimate of the percent error in the proton flux.  The percent error is defined
  as a relative error: d(Flux)/Flux, where Flux is the proton flux.
  

  ---> FPSA Quality flag [FPSA_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  FPDU: Unidirectional Differential Proton Flux ~50-1500 keV, in up to 31 energy and 64 sector bins (energy-sector displays) [FPDU]

  Unidirectional Differential Proton Flux (FPDU). Dimension 1 is for the 31 magEIS
  energy channels. The energy channel centroids are specified in FPDU_Energy. The
  channel widths are specified in FPDU_Energy_Widths.If less than 31 channels are
  used the remaining channel dimensions are set to fill values. Dimension 2 is for
  the 64 sector angles. Here, the dimension size of 64 is the maximum number of
  possible sectors. If less than 64 are being used, the data are set to fill
  values of -1.0E31. The sector angle values for valid (non-fill) sectors are
  given in FPDU_Sector_Angle.
  

  ---> Spectrograms by sector at sample energies [FPDU_E]
  ---> Spectrograms by energy at sample sectors [FPDU_A]
  ---> [NO PLOTS] % error in FPDU [FPDU_ERROR]

  Estimate of the percent error in the proton flux.  The percent error is defined
  as a relative error: d(Flux)/Flux, where Flux is the proton flux.
  

  ---> [NO PLOTS] FPDU Quality flag [FPDU_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  ---> [NO PLOTS] FPDU Quality flag (Full bitmap) [FPDU_Quality_FULL]

  32-bit flag position. Quality flag is a long int. This is the bit-position that
  is set (from right to left).....0,Background correction was not done (main
  channels).1,The test pulser was on at the current time..2,The detector biases
  were disabled at the current time..3,An engineering look-up-table was used for
  the main and/or derived channel data at the current time. NOTE THAT THE CHANNEL
  MAPPING IS INVALID HERE..4,The front detectors were selected at the current time
  (high unit electron only)..5,The data was set to fill as instructed by the
  calibration file..6,There was no housekeeping and/or digital status data found.
  The bias status, pulser status, etc... is not known..7,There are no main
  channels defined at the current time.8,There are no derived channels defined at
  the current time.9,A validity check failed in the flux conversion. This usually
  indicates that an engineering look-up-table was selected at the current
  time..10,A calibration file could not be found for the current look-up-table ID.
  NOTE THAT THE CHANNEL MAPPING IS INVALID HERE..11,Data was not found at the
  current time for at least one of LOW, MED, HIGH (defined for combined L2 product
  only).12,These channels are not defined for this pixel (HIGH proton only).13,The
  coincidence was disabled at the current time (high unit electron
  only)..14,Livetime correction not applied (main rate): Unknown reason.15,dQ/Q
  greater-than 0.5; Warning. Counts are low and/or error estimate is
  large.16,Livetime correction not applied (histogram): Unknown
  reason.17,Background correction was not done (derived channels).18,The number of
  sectors changed (nsectors)..19,The accumulation interval changed
  (nspins)..20,The LUT changed..21,Livetime correction not applied (main rate):
  The livetime value failed the valid bounds check. This indicates an issue and
  the data is set to fill..22,Livetime correction not applied (main rate):
  pixel-to-channel mapping is invalid.23,Livetime correction not applied (main
  rate): nsectors_main not equal to nsectors_LT.24,Livetime correction not applied
  (main rate): next METs not equal.25,Livetime correction not applied (main rate):
  matching METs not found.26,Livetime correction not applied (main rate): could
  not determine if front or rear detectors were selected (HIGH electron data
  only).27,Livetime correction applied, with warning (main rate): min LT in this
  spin is less than 60%.28,Livetime correction not applied (main rate): no LT
  data.29,dQ/Q greater-than 1.0; Warning. Counts are very low and/or error
  estimate is very large.30,Unit is in sample mode at the given time (i.e.
  background corrections cannot be done)..31,UNUSED
  

  Flag to indicate whether or not the electron coincidence is enabled (0=disabled; 1=enabled). [COINCIDENCE_MODE]

  Flag to indicate whether or not the electron coincidence is enabled (0=disabled;
  1=enabled). This variable is only defined for the HIGH unit (~850-4000 keV), as
  this is the only MagEIS unit with coincidence. In the disabled coincidence
  state, the electron fluxes should only be used qualitatively, and with caution.
  

  ---> Flag to indicate mode of the MagEIS instruments (0=maintenance; 1=science; 2=high rate). [INSTRUMENT_MODE]

  Flag to indicate mode of the MagEIS instruments (0=maintenance; 1=science;
  2=high rate). Only the LOW and MED units (~20-1000 keV) can go into high rate
  mode. The HIGH unit (~850-4000 keV), can only be in maintenance or science mode.
  The most common reason why background corrections cannot be done (e.g.
  FESA_CORR, FEDU_CORR are fill) is when the LOW and/or MED units are in high-rate
  mode.
  

  ---> Flag to indicate whether or not the electron detectors are in the normal-bias or low-bias state (0=low bias; 1=normal bias) [BIAS_MODE]

  Flag to indicate whether or not the electron detectors are in the normal-bias or
  low-bias state (0=low bias; 1=normal bias). In the low-bias state, the electron
  fluxes should only be used qualitatively, and with caution.
  

  ---> Ratio of the background estimate divided by the main rate rate, for the spin-averaged data. [BKG_TO_MAIN_RATIO_SPINAVG]

  Ratio of the background estimate divided by the main rate rate, for the
  spin-averaged data. This gives an estimate of the level of background
  contamination in the main rate data (large % = high background) and/or how close
  the main rate data is to the background level (large % = low counts).
  

  [Time-series] Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates [Position_TT]
  ---> Calculated magnetic field strength [B_Calc_TT]
  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]
  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]
  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]
  ---> Adiabatic invariant (bounce) [I_TT]
  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

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RBSPA_REL03_ECT-REPT-SCI-L2 doi:10.48322/hpp2-yy26 Copy BibTeX Citation

Description

RBSP Relativistic Electron Proton Telescope, Level 2 science data

Modification History

CDF skeleton version of rbsp_rept_science_l2_data.template.cdf written by R.
Reukauf

• Data Variable Descriptions
  Data Quality Flag (0=valid) [Data_Quality]

  0 = valid data; 1 = timing err; 2 = bias_st off; 3 = timing err and bias_st off
  

  FESA: Spin-Averaged Differential Electron Flux 2-20 MeV, in 12 energy bands (spectrogram) [FESA]

  Dimension 1 corresponds to 12 electron energy bins.
  

  ---> (stacked time series) [FESA_E]

  Dimension 1 corresponds to 12 electron energy bins.
  

  FEDU: Unidirectional Differential Electron Flux 2-20 MeV, in 12 energy and 36 angle bins (energy-angle displays) [FEDU]

  Dimension 1 corresponds to 12 electron energy bins.  Dimension 2 holds 36
  sectors.
  

  ---> Spectrograms by energy at sample angles [FEDU_E]
  ---> Spectrograms by angle at sample energies [FEDU_A]

  Dimension 1 corresponds to 12 electron energy bins.  Dimension 2 holds 36
  sectors.
  

  FPSA: Spin-Averaged Differential Proton Flux 20-120 MeV (spectrograms) [FPSA]

  Dimension 1 corresponds to 8 proton energy bins.
  

  ---> (stacked time series) [FPSA_E]

  Dimension 1 corresponds to 8 proton energy bins.
  

  FPDU - Unidirectional Differential Proton Flux 20-120 MeV, in 8 energy and 36 angle bins (energy-angle displays) [FPDU]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  ---> Spectrograms in energy at sample angles [FPDU_E]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  ---> Spectrograms in angle at sample energies [FPDU_A]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  [Time-series] Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates [Position_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc_TT]
  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]
  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]
  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]
  ---> Adiabatic invariant (bounce) [I_TT]
  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

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RBSPA_REL03_ECT-REPT-SCI-L3 doi:10.48322/4x5t-th95 Copy BibTeX Citation

Description

Van Allen Probes, RBSPECT/REPT (Radiation Belt Storm Probes Energetic particle,
Composition and Thermal plasma suite/Relativistic Electron Proton Telescope,
Level 3 Pitch Angle Sorted Data.

• Data Variable Descriptions
  FEDU - Unidirectional Differential Electron Flux [FEDU]

  Dimension 0 holds 7910 time bins. Dimension 1 corresponds to 17 pitch angle
  bins.  Dimension 2 holds 8 energy bins.
  

  ---> FEDU_byE_atA: Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> FEDU_byA_atE: Spectrograms by pitch angle at sample energies [FEDU_byA_atE]
  FPDU - Unidirectional Differential Proton Flux [FPDU]

  Dimension 0 holds 7910 time bins. Dimension 1 corresponds to 17 pitch angle
  bins.  Dimension 2 holds 8 energy bins.
  

  ---> FPDU_byE_atA: Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> FPDU_byA_atE: Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  FEDU_0to180 - Unidirectional Differential Electron Flux [FEDU_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms at sample pitch angles [FEDU_0to180_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_0to180_byA_atE]
  FEDU_180to360 - Unidirectional Differential Electron Flux [FEDU_180to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_180to360_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_180to360_byA_atE]
  FPDU_0to180 - Unidirectional Differential Proton Flux [FPDU_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_0to180_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_0to180_byA_atE]
  FPDU_180to360 - Unidirectional Differential Proton Flux [FPDU_180to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_180to360_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_180to360_byA_atE]
  FEDU_Unbinned_0to180 - Unidirectional Differential Electron Flux (raw sector data). [FEDU_Unbinned_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 12 energy bins.
  

  ---> FEDU_Unbinned_0to360 - Unidirectional Differential Electron Flux (raw sector data). [FEDU_Unbinned_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 12 energy bins.
  

  FPDU_Unbinned_0to180 - Unidirectional Differential Proton Flux (raw sector data). [FPDU_Unbinned_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 8 energy bins.
  

  ---> FPDU_Unbinned_0to360 - Unidirectional Differential Proton Flux (raw sector data). [FPDU_Unbinned_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 8 energy bins.
  

  [NO PLOTS] FPDU_Unbinned_LightMask_0to360 - LightMask for FPDU_Unbinned_0to360 array. [FPDU_Unbinned_LightMask_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins.
  

  ---> FPDU_Unbinned_Light_Flag [FPDU_Unbinned_Light_Flag]

  Dimensions 0 holds 7910 time bins. 
  

  Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT]
  ---> Position in geocentric Geographic coords [Position]
  [TEXT LABELS] Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star_TT]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_TT]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT_TT]
  ---> Position in geocentric Geographic coords [Position_TT]

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RBSPA_REL04_ECT-HOPE-MOM-L3 doi:10.48322/egeg-7005 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by B. Larsen.20140304

• Data Variable Descriptions
  HOPE proton parallel temperature [Tpar_p_30]

  Temperature for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He+ parallel temperature [Tpar_he_30]

  Temperature for he as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE O+ parallel temperature [Tpar_o_30]

  Temperature for o as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE electron parallel temperature [Tpar_e_200]

  Temperature for e as a function of time for apogee mode only from 200 eV energy
  up
  

  HOPE proton perpendicular temperature [Tperp_p_30]

  Temperature for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He+ perpendicular temperature [Tperp_he_30]

  Temperature for he as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE O+ perpendicular temperature [Tperp_o_30]

  Temperature for o as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE electron perpendicular temperature [Tperp_e_200]

  Temperature for e as a function of time for apogee mode only from 200 eV energy
  up
  

  HOPE proton Tperp/Tpar [Tperp_Tpar_p_30]

  Tperp on Tpar for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He Tperp/Tpar [Tperp_Tpar_he_30]

  Tperp on Tpar for he as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE Oxygen Tperp/Tpar [Tperp_Tpar_o_30]

  Tperp over Tpar for o as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE electron Tperp/Tpar [Tperp_Tpar_e_30]

  Tperp over Tpar for e as a function of time for apogee mode only from 30 eV
  energy up
  

  HOPE ion partial density [Ion_density]

  Partial ion density as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE proton partial density [Dens_p_30]

  Partial density for p as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE He+ partial density [Dens_he_30]

  Partial density for he as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE O+ partial density [Dens_o_30]

  Partial density for o as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE electron partial density [Dens_e_200]

  Partial density for e as a function of time for apogee mode only from 200 eV
  energy up
  

  HOPE He/p partial density ratio [he_p_ratio]

  Partial density ratio for he/p as a function of time for apogee mode only from
  30 eV energy up
  

  ---> HOPE He/Oxygen partial density ratio [he_o_ratio]

  Partial density ratio for He/O as a function of time for apogee mode only from
  30 eV energy up
  

  ---> HOPE Oxygen/proton partial density ratio [o_p_ratio]

  Partial density ratio for o/p as a function of time for apogee mode only from 30
  eV energy up
  

  Quality Flag for proton temperatures [p_T_flag]

  Flag that is set for suspicious temperature values for p
  

  ---> Quality Flag for He temperatures [he_T_flag]

  Flag that is set for suspicious temperature values for he
  

  ---> Quality Flag for Oxygen temperatures [o_T_flag]

  Flag that is set for suspicious temperature values for o
  

  ---> Quality Flag for electron temperatures [e_T_flag]

  Flag that is set for suspicious temperature values for e
  

  Quality Flag for proton Tperp consistency [p_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for p
  

  ---> Quality Flag for He Tperp consistency [he_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for
  he
  

  ---> Quality Flag for Oxygen Tperp consistency [o_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for o
  

  ---> Quality Flag for electron Tperp consistency [e_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for e
  

  Quality Flag for proton density [p_Dens_flag]

  Flag that is set for suspicious density values for p
  

  ---> Quality Flag for He density [he_Dens_flag]

  Flag that is set for suspicious density values for he
  

  ---> Quality Flag for Oxygen density [o_Dens_flag]

  Flag that is set for suspicious density values for o
  

  ---> Quality Flag for electron density [e_Dens_flag]

  Flag that is set for suspicious density values for e
  

  Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Position of the satellite in geographic coordinates [Position_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

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RBSPA_REL04_ECT-HOPE-PA-L3 doi:10.48322/17p9-rf75 Copy BibTeX Citation

Description

Pitch angle binned data from the HOPE plasma spectrometer.  Note that there are
no correections performed on the data (e.g. background subtraction, velocity
corrections, etc.)

Modification History

CDF skeleton version of 20120705. Written by R. Friedel.
20120706 version written by R. Skoug. 
20130715 revisions by J. T. Niehof.
20130808 revisions by J. T. Niehof/BA Larsen.
20130927 revision (remove per-mode variables)by J. T. Niehof.

• Data Variable Descriptions
  FEDO: Omnidirectional differential electron flux ~15-50,000 eV [FEDO]

  Electron flux integrated (piecewise constant) over pitch angle (11) and gyro
  angle (20) as computed from magnetic field direction crossed with spacecraft
  spin axis and energy (72).  Note that data have been expanded to the highest
  possible resolution, even though before 9/2013 the transmitted data are
  collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigee mode excluded) [FEDO_T]

  Electron flux integrated (piecewise constant) over pitch angle (11) and gyro
  angle (20) as computed from magnetic field direction crossed with spacecraft
  spin axis and energy (72).  Note that data have been expanded to the highest
  possible resolution, even though before 9/2013 the transmitted data are
  collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FEDU: Unidirectional Differential Electron Flux ~15-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FEDU]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles (perigee mode excluded) [FEDU_byE_atA]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigee mode excluded) [FEDU_byA_atE]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FPDO: Omnidirectional differential Proton flux ~1-50,000 eV [FPDO]

  Proton flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FPDO_T]

  Proton flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FPDU: Unidirectional Differential Proton Flux ~1-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FPDU]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FPDU_byA_atE]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FODO: Omnidirectional differential Oxygen flux ~1-50,000 eV [FODO]

  Oxygen flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FODO_T]

  Oxygen flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FODU: Unidirectional Differential Oxygen Flux ~1-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FODU]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FODU_byA_atE]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FHEDO: Omnidirectional differential Helium flux ~1-50,000 eV [FHEDO]

  Helium flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FHEDO_T]

  Helium flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FHEDU: Unidirectional Differential Helium Flux ~1-50,000 keV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FHEDU]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FHEDU_byE_atA]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FHEDU_byA_atE]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  Flags on electron data [Flags_Ele]

  Flags to indicate potential issues with electron data. Each element of this
  array contains the flag status for a particular concern. A flag value of zero
  indicates no unusual concerns of that type for that time sample. Increasing flag
  values indicate increasing concern. See FLAGS variable for a description of each
  element.
  

  ---> Flags on ion data [Flags_Ion]

  Flags to indicate potential issues with electron data. Each element of this
  array contains the flag status for a particular concern. A flag value of zero
  indicates no unusual concerns of that type for that time sample. Increasing flag
  values indicate increasing concern. See FLAGS variable for a description of each
  element.
  

  Mode of electron data [Mode_Ele]

  Indicates instrument mode for electron data. Each mode has a different set of
  energy channels. See corresponding HOPE_ENERGY_Ion record. (0) Apogee mode:
  normal operation. (1) Perigee mode: minimum energy channel raised during pass
  through perigee. (2) burst mode: subset of energies sampled at rapid cadence.
  

  ---> Mode of ion data [Mode_Ion]

  Indicates instrument mode for ion data. Each mode has a different set of energy
  channels. See corresponding HOPE_ENERGY_Ion record. (0) Apogee mode: normal
  operation. (1) Perigee mode: minimum energy channel raised during pass through
  perigee.
  

  HOPE electron counts OMNI [Counts_E_Omni]

  Electron counts summed over pitch angle (11) and gyro angle (20) as computed
  from magnetic field direction crossed with spacecraft spin axis and energy (72).
   Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE electron counts directional [Counts_E]

  Electron counts as a function of pitch angle (11) as computed from magnetic
  field direction crossed with spacecraft spin axis and energy (72).  Note that
  data have been expanded to the highest possible resolution, even though before
  9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles)
  to fit the telemetry allocation. Counts are summed over all measurements in a
  PA/gyro bin.
  

  HOPE proton counts OMNI [Counts_P_Omni]

  Proton counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE proton counts directional [Counts_P]

  Proton counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  HOPE helium counts OMNI [Counts_He_Omni]

  Helium counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE helium counts directional [Counts_He]

  Helium counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  HOPE Oxygen counts OMNI [Counts_O_Omni]

  Oxygen counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE Oxygen counts directional [Counts_O]

  Oxygen counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
Back to top

---

RBSPA_REL04_ECT-HOPE-SCI-L2 doi:10.48322/34q8-8q26 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by R. Friedel..20120706 version,
written by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written
by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written by R.
Skoug.20130715 revisions by J. T. Niehof
20120706 version, written by R. Skoug
20130715 revisions by J. T. Niehof

• Data Variable Descriptions
  Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to ion measurement timebase from 1 min. resolution
  MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates(ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  Detector No. [HOPE_DETECTOR]
  Sector No. [HOPE_SECTOR]
  [CreateCDF ONLY] FPDU: Differential directional proton flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FPDU]

  Proton flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FPDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D5_BY_ENERGY]
  ---> FPDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D5_BY_ANGLE]
  [CreateCDF ONLY] FHeDU: Differential directional helium flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FHEDU]

  Helium flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 3-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FHeDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D5_BY_ENERGY]
  ---> FHeDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D5_BY_ANGLE]
  [CreateCDF ONLY] FODU: Differential directional oxygen flux ~1-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FODU]

  Oxygen flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FODU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D5_BY_ENERGY]
  ---> FODU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D5_BY_ANGLE]
  [CreateCDF ONLY] FEDU: Differential directional electron flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FEDU]

  Electron flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FEDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D5_BY_ENERGY]
  ---> FEDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D5_BY_ANGLE]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
Back to top

---

RBSPA_REL04_ECT-HOPE-SCI-L2SA doi:10.48322/rcxw-mm23 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by R. Friedel..20120706 version,
written by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written
by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written by R.
Skoug.20130715 revisions by J. T. Niehof
20120706 version, written by R. Skoug
20130715 revisions by J. T. Niehof

• Data Variable Descriptions
  Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to ion measurement timebase from 1 min. resolution
  MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates(ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  Detector No. [HOPE_DETECTOR]
  Sector No. [HOPE_SECTOR]
  HOPE Spin averaged differential oxygen flux (as spectrogram) [FOSA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FOSA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential proton flux [FPSA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FPSA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential helium flux [FHESA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FHESA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential electron flux [FESA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time_series [FESA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

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RBSPA_REL04_ECT-MAGEIS-L3 doi:10.48322/09qz-tf17 Copy BibTeX Citation

Description

Van Allen Probes, RBSPECT/MagEIS (Radiation Belt Storm Probes Energetic
particle, Composition and Thermal plasma suite/Magnetic Electron Ion
Spectrometer, Level 3 Pitch Angle Sorted Data.

• Data Variable Descriptions
  FEDU: Unidirectional Differential Electron Flux, ~20-4000 keV in 23 energy and 11 pitch angle bins (energy-angle displays) [FEDU_plasmagram]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  [Movie] FEDU: Unidirectional Differential Electron Flux, ~20-4000 keV in 23 energy and 11 pitch angle bins (energy-angle displays) [FEDU_plasmagram_movie]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by pitch angle at sample energies [FEDU_byA_atE]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> FEDU_ERROR - sqrt of Unidirectional Differential Electron Counts [FEDU_ERROR]

  Dimension 0 holds 7805 time bins. Dimension 1 corresponds to 11 pitch angle
  bins.  Dimension 2 holds 25 energy bins.
  

  FEDU_CORR - Background-Corrected Unidirectional Differential Electron Flux [FEDU_CORR_plasmagram]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  [Movie] FEDU_CORR - Background-Corrected Unidirectional Differential Electron Flux [FEDU_CORR_plasmagram_movie]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_CORR_byE_atA]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> Spectrograms by pitch angle at sample energies [FEDU_CORR_byA_atE]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> FEDU_CORR_ERROR - Estimate of the percent error in the corrected electron flux. [FEDU_CORR_ERROR]

  Dimension 0 holds 8011 time bins. Dimension 1 corresponds to 11 pitch angle
  bins.  Dimension 2 holds 25 energy bins. The percent error is defined as a
  relative error: d(Flux)/Flux*100%, where Flux is the corrected flux.
  

  FPDU: Unidirectional Differential Proton Flux, ~60-1300 keV in 21 energy and 32 pitch angle bins (energy-angle displays) [FPDU_plasmagram]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  [Movie] FPDU: Unidirectional Differential Proton Flux, ~60-1300 keV in 21 energy and 32 pitch angle bins (energy-angle displays) [FPDU_plasmagram_movie]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  FDPU_pix1 - Unidirectional Differential Proton Flux [FPDU_pix1]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  ---> [Movie] FDPU_pix1 - Unidirectional Differential Proton Flux [FPDU_pix1_movie]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  FDPU_pix2 - Unidirectional Differential Proton Flux [FPDU_pix2]

  Dimension 0 holds 7918 time bins. Dimension 1 corresponds to 15 pitch angle
  bins.  Dimension 2 holds 31 energy bins.
  

  ---> [Movie] FDPU_pix2 - Unidirectional Differential Proton Flux [FPDU_pix2_movie]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star]

  L-shell parameters are dimensionless.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L]

  L-shell parameters are dimensionless.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I]
  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc]
  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq]
  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT]
  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT]
  ---> Position - Geocentric Geocentric position in Re. [Position]
  ---> LstarVsAlpha - Roederer's generalized L-shell parameter. Pitch angle depenedent (pitch angles are local pitch angles). Computed using OP77Q external field and IGRF internal field. [LstarVsAlpha]

  L-shell parameters are dimensionless.
  

  ---> Alpha values for LstarVsAlpha variable. I.e., they are the local pitch angles that L* is computed for in LstarVsAlpha. Units are degrees. [LstarVsAlpha_Alpha]

  Alpha values for LstarVsAlpha variable.
  

  [Labels on plots] Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star_TT]

  L-shell parameters are dimensionless.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_TT]

  L-shell parameters are dimensionless.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I_TT]
  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc_TT]
  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq_TT]
  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT_TT]
  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT_TT]
  ---> Position - Geocentric Geocentric position in Re. [Position_TT]

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RBSPB_EFW-L2_E-HIRES-UVW doi:10.48322/64bn-y776 Copy BibTeX Citation

Description

High Resolution DC Electric Field in UVW Coordinates.

Modification History

v01:  initial version.

• Data Variable Descriptions
  Efield (UVW) [e_hires_uvw]

  DC electric field in the UVW coordinate system at 16 or 32 samples/sec
  

  Efield raw (UVW) [e_hires_uvw_raw]

  DC electric field in the UVW coordinate system at 16 or 32 samples/sec, without
  spinning-frame offset removal
  

  Spin Axis Vector in GSE [L_vector]

  Angular momentum/spin axis direction of spacecraft spin, namely, the sunward
  pointing direction of spacecraft spin axis.
  

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RBSPB_EFW-L2_E-SPINFIT-MGSE doi:10.48322/s0hb-rp21 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spaceraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

• Data Variable Descriptions
  Spinfit E-field in MGSE (autoscale, VxB subtracted, i.e. near GSE) [efield_spinfit_mgse]

  Spin-fit electric field esimate in the MGSE coordinate system and GSE frame (VxB
  subtracted) derived from the EFW e12 (V1-V2) data product.
  

  ---> Spinfit E-field in MGSE (fixedscale, VxB subtracted, i.e. near GSE) [efield_spinfit_mgse_fixedscale]

  Spin-fit electric field esimate in the MGSE coordinate system and GSE frame (VxB
  subtracted) derived from the EFW e12 (V1-V2) data product.
  

  VxB E-field in MGSE coordinates. [VxB_mgse]

  Electric field due to VxB, where V is spacecraft velocity and B is the measured
  ambient magnetic field.
  

  ---> Corotation Efield (MGSE) [efield_coro_mgse]

  Corotation electric field
  

  EFW quality array (global estimate of EFW data quality, plus 13 underlying observatory and instrument-level data quality factors) [e_spinfit_mgse_efw_qual]
  Bias current [bias_current]

  Bias current (nA) applied to the antenna probes
  

  L_vector (spin axis GSE) [spinaxis_gse]

  Unit vector of spin axis (w) in the GSE coordinate system, also the pointing
  direction defining the spacecraft angular velocity
  

  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [flags_all]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_DUNNO (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

  ---> MLT [mlt]

  Spacecraft magnetic local time in hour
  

  ---> MLat [mlat]

  Spacecraft magnetic latitude in deg
  

  ---> L [lshell]

  Spacecraft L-shell from simple dipole model
  

  ---> Lstar [Lstar]

  Lstar
  

  S/C position in GSE [pos_gse]

  Spacecraft position in km in the GSE coordinate system
  

  ---> S/C velocity in GSE [vel_gse]

  Spacecraft velocity in km/s in the GSE coordinate system
  

  ---> Orbit number [orbit_num]

  orbit number
  

  Angles b/t the Ey and Ez MGSE spinplane directions and the background magnetic field. [angle_Ey_Ez_Bo]

  Angle b/t the Ey(Ez) MGSE spinplane directions and the background magnetic
  field. Used to test when the E*B=0 assumption is appropriate
  

  diagEx1 [diagEx1]

  Diagnostic quantity 1 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagEx2 [diagEx2]

  Diagnostic quantity 2 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagBratio [diagBratio]

  Diagnostic variable with By/Bx and Bz/Bx for the E*B=0 calculation
  

  flags_charging_bias_eclipse [flags_charging_bias_eclipse]

  charging, bias, eclipse flags, extreme charging
  

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RBSPB_EFW-L2_ESVY_DESPUN doi:10.48322/036a-q517 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spaceraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

• Data Variable Descriptions
  Despun E-field in MGSE (32 S/s, VxB subtracted, near GSE) [efield_mgse]

  Electric field in the MGSE coordinate system (Vsc x B subtracted) at 16 or 32
  samples/sec.
  

  ---> EFW quality array (global estimate of EFW data quality, plus 13 underlying observatory and instrument-level data quality factors) [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_flags_all is a collection of flags that show
  the estimate of each of these contributors over time.    See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_flags_all.  If the
  value of a particular element of efw_flags_all is not relevant to the quality of
  a particular data product, it shall receive the value EFW_FLAGS_NR (typ. -2). 
  If the value of a particular element of efw_flags_all is relevant to the quality
  of a particular data product but is not known at the time of data production, it
  shall receive the value EFW_FLAGS_DUNNO (typ. -1).  A quality value of
  EFW_FLAGS_GOOD (typ. 0) indicates that there are no known issues with the data
  product due to that particular element of efw_flags_all.  The quality values are
  meant to be conservative, and values other than EFW_FLAGS_GOOD should lead the
  user back to a member of the EFW instrument team for discussion and advice on
  the nature of the data quality as needed.
  

  orbit_num [orbit_num]

  orbit number
  

  MLT [mlt]

  Magnetic local time from ECT's predicted Ephemeris
  

  ---> Mlat [mlat]

  Magnetic latitude from ECT's predicted Ephemeris
  

  ---> Lshell (simple dipole, from ECT predicted Ephermis) [lshell]

  Simple dipole Lshell from ECT's predicted Ephemeris
  

  ---> GSE position [pos_gse]

  GSE position in km from SPICE
  

  ---> GSE velocity [vel_gse]

  GSE velocity in km/s from SPICE
  

  L_vector [spinaxis_gse]

  Pointing direction (GSE) defining the spacecraft angular velocity (spinaxis w
  component)
  

  bias_current [bias_current]

  Bias current (nA) applied to the antenna probes 
  

  diagEx1 [diagEx1]

  Diagnostic quantity 1 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagEx2 [diagEx2]

  Diagnostic quantity 2 from the E*B=0 calculation. Spin-fit electric field
  calculation in the MGSE coordinate system. The Vsc x B field is subtracted off,
  where Vsc is the spacecraft velocity and B is the measured ambient magnetic
  field.
  

  diagBratio [diagBratio]

  Diagnostic variable with By/Bx and Bz/Bx for the E*B=0 calculation
  

  flags_charging_bias_eclipse [flags_charging_bias_eclipse]

  charging, bias, eclipse, extreme charging flags
  

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RBSPB_EFW-L2_FBK doi:10.48322/m9dn-c472 Copy BibTeX Citation

Description

Up to two sources are returned. The possible sources are:
E12DC, E34DC,E56DC,
E12AC,E34AC,E56AC,
SCMU,SCMV,SCMW
(V1DC+V2DC+V3DC+V4DC)/4

• Data Variable Descriptions
  Filterbank 13 (<=2013 Mar16) E12DC peak values [fbk13_e12dc_pk]
  ---> Low frequency values overlaid [fbk13_e12dc_pk_lowoverlay]
  Filterbank 13 E34DC peak values [fbk13_e34dc_pk]
  Filterbank 13 (<=2013 Mar16) SCMw peak values [fbk13_scmw_pk]
  ---> Low frequency values overlaid [fbk13_scmw_pk_lowoverlay]
  Filterbank 13 (<=2013 Mar16) E12DC average values [fbk13_e12dc_av]
  ---> Low frequency values overlaid [fbk13_e12dc_av_lowoverlay]
  Filterbank 13 E34DC average values [fbk13_e34dc_av]
  Filterbank 13 (<=2013 Mar16) SCMw average values [fbk13_scmw_av]
  ---> Low frequency values overlaid [fbk13_scmw_av_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) E12DC peak values [fbk7_e12dc_pk]
  ---> Low frequency values overlaid [fbk7_e12dc_pk_lowoeverlay]
  Filterbank 7 (Early 2012) SCMu peak values [fbk7_scmu_pk]
  Filterbank 7 (>=2013 Mar 17) SCMw peak values [fbk7_scmw_pk]
  ---> Low frequency values overlaid [fbk7_scmw_pk_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) E12DC average values [fbk7_e12dc_av]
  Filterbank 7 (Early 2012) SCMu average values [fbk7_scmu_av]
  ---> Low frequency values overlaid [fbk7_e12dc_av_lowoverlay]
  Filterbank 7 (>=2013 Mar 17) SCMw average values [fbk7_scmw_av]
  ---> Low frequency values overlaid [fbk7_scmw_av_lowoverlay]
  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_UNK (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

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RBSPB_EFW-L2_SPEC doi:10.48322/hdnm-mh60 Copy BibTeX Citation

Description

Six spectral products are returned. The possible sources
are:.E12dc,E34dc,E56dc.E12ac,E34ac,E56ac.Edcpar,Edcprp.Eacpar,Eacprp.V1ac,V2ac,V
3ac,V4ac,V5ac,V6ac.SCMU,SCMV,SCMW.SCMpar,SCMprp,.(V1ac+V2ac+V3ac+V4ac)/4,.Edcprp
2, Eacprp2, SCMprp2.

Caveats

See THEMIS website for caveats

• Data Variable Descriptions
  E12 AC [spec64_e12ac]

  64 bin spectrogram for E12AC
  

  spec64_e12dc [spec64_e12dc]

  64 bin spectrogram for E12DC
  

  ---> E56 AC [spec64_e56ac]

  64 bin spectrogram for E56AC
  

  spec64_e34dc [spec64_e34dc]

  64 bin spectrogram for E34DC
  

  [64 FREQUENCIES] V1 AC [spec64_v1ac]

  64 bin spectrogram for V1AC
  

  spec64_e34ac [spec64_e34ac]

  64 bin spectrogram for E34AC
  

  ---> V2 AC [spec64_v2ac]

  64 bin spectrogram for V2AC
  

  spec64_e56dc [spec64_e56dc]

  64 bin spectrogram for E56DC
  

  [64 FREQUENCIES] SCM u [spec64_scmu]

  64 bin spectrogram for SCMu
  

  ---> SCM v [spec64_scmv]

  64 bin spectrogram for SCMv
  

  spec64_epar_dc [spec64_epardc]

  64 bin spectrogram for Eparallel DC
  

  ---> SCM w [spec64_scmw]

  64 bin spectrogram for SCMw
  

  spec64_eperp1dc [spec64_eperp1dc]

  64 bin spectrogram for Eperp1 DC
  

  spec64_eparac [spec64_eparac]

  64 bin spectrogram for Eparallel AC
  

  spec64_eperp1ac [spec64_eperp1ac]

  64 bin spectrogram for Eperp1 AC
  

  An array that indicates a global estimate of EFW data quality, as well as a breakdown of observatory and instrument-level data quality issues that impact the global quality estimate.. [efw_qual]

  The quality of EFW data products can be affected by a variety of observatory and
  instrument-level conditions.  efw_qual is a collection of flags that show the
  estimate of each of these contributors over time.  ..See the EFW-FAQ
  (http://rbsp.space.umn.edu/efw_faq.html) for a detailed description of the 
  determination and meaning of each of the elements of efw_qual...If the value of
  a particular element of efw_qual is not relevant to the quality of a particular
  data product, it shall receive the value EFW_QUAL_NR (typ. -2)...If the value of
  a particular element of efw_qual is relevant to the quality of a particular data
  product but is not known at the time lf L2 data production, it shall receive the
  value EFW_QUAL_UNK (typ. -1)...A quality value of EFW_QUAL_GOOD (typ. 0)
  indicates that there are no known issues with the data product due to that
  particular element of efw_qual...The quality values are meant to be
  conservative, and values other than EFW_QUAL_GOOD should lead the user back to a
  member of the EFW instrument team for discussion and advice on the nature of the
  data quality as needed.
  

  spec64_v3ac [spec64_v3ac]

  64 bin spectrogram for V3AC
  

  spec64_v4ac [spec64_v4ac]

  64 bin spectrogram for V4AC
  

  spec64_v5ac [spec64_v5ac]

  64 bin spectrogram for V5AC
  

  spec64_v6ac [spec64_v6ac]

  64 bin spectrogram for V6AC
  

  spec64_scmpar [spec64_scmpar]

  64 bin spectrogram for SCMpar
  

  spec64_scmperp1 [spec64_scmperp1]

  64 bin spectrogram for SCMperp1
  

  spec64_v1234_avg [spec64_v1234_avg]

  64 bin spectrogram for (v1+v2+v3+v4)/4
  

  spec64_eperp2dc [spec64_eperp2dc]

  64 bin spectrogram for Eperp2 DC
  

  spec64_eperp2ac [spec64_eperp2ac]

  64 bin spectrogram for Eperp2 AC
  

  spec64_scmperp2 [spec64_scmperp2]

  64 bin spectrogram for SCMperp2
  

  spec36_e12dc [spec36_e12dc]
  spec36_e12ac [spec36_e12ac]
  spec36_e34dc [spec36_e34dc]
  spec36_e34ac [spec36_e34ac]
  spec36_e56dc [spec36_e56dc]
  spec36_e56ac [spec36_e56ac]
  spec36_epardc [spec36_epardc]
  spec36_eperp1dc [spec36_eperp1dc]
  spec36_eparac [spec36_eparac]
  spec36_eperp1ac [spec36_eperp1ac]
  spec36_v1ac [spec36_v1ac]
  spec36_v2ac [spec36_v2ac]
  spec36_v3ac [spec36_v3ac]
  spec36_v4ac [spec36_v4ac]
  spec36_v5ac [spec36_v5ac]
  spec36_v6ac [spec36_v6ac]
  spec36_scmu [spec36_scmu]
  spec36_scmv [spec36_scmv]
  spec36_scmw [spec36_scmw]
  spec36_scmpar [spec36_scmpar]
  spec36_scmperp1 [spec36_scmperp1]
  spec36_v1234_avg [spec36_v1234_avg]
  spec36_eperp2dc [spec36_eperp2dc]
  spec36_eperp2ac [spec36_eperp2ac]
  spec36_scmperp2 [spec36_scmperp2]
  spec112_e12dc [spec112_e12dc]
  spec112_e12ac [spec112_e12ac]
  spec112_e34dc [spec112_e34dc]
  spec112_e34ac [spec112_e34ac]
  spec112_e56dc [spec112_e56dc]
  spec112_e56ac [spec112_e56ac]
  spec112_epardc [spec112_epardc]
  spec112_eperp1dc [spec112_eperp1dc]
  spec112_eparac [spec112_eparac]
  spec112_eperp1ac [spec112_eperp1ac]
  spec112_v1ac [spec112_v1ac]
  spec112_v2ac [spec112_v2ac]
  spec112_v3ac [spec112_v3ac]
  spec112_v4ac [spec112_v4ac]
  spec112_v5ac [spec112_v5ac]
  spec112_v6ac [spec112_v6ac]
  spec112_scmu [spec112_scmu]
  spec112_scmv [spec112_scmv]
  spec112_scmw [spec112_scmw]
  spec112_scmpar [spec112_scmpar]
  spec112_scmperp1 [spec112_scmperp1]
  spec112_v1234_avg [spec112_v1234_avg]
  spec112_eperp2dc [spec112_eperp2dc]
  spec112_eperp2ac [spec112_eperp2ac]
  spec112_scmperp2 [spec112_scmperp2]

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RBSPB_EFW-L2_VSVY-HIRES doi:10.48322/e9bt-8x09 Copy BibTeX Citation

Description

CDAWeb interface derived data on Fri Jun 14 15:33:16 EDT 2013. Contacts: 
Tami.J.Kovalick@nasa.gov, Rita.C.Johnson@nasa.gov. Spinfit DC electric field
estimates in the M-GSE coordinate system - see the EFW-FAQ
(http://rbsp.space.umn.edu/efw_faq.html) for a description of the spin fit 
algorithm and the M-GSE coordinate system.
One 2D vector estimate of the E-field is computed at a cadence of once per spin
period (typ. 10.7 to 11.1 s) using the survey E-field data product - the
potential difference between EFW sensors V1 and V2 (E12) or V3 and V4 (E34)
sampled at a nominal rate of 32 samp/s with a resolution of 16 bits.
The X-component of the E-field estimate, corresponding to the axial component in
the spacecraft coordinate system, is set to zero in this data product.  See the
EFW-FAQ (http://rbsp.space.umn.edu/efw_faq.html) for a discussion of this 
convention for this data product.
The VxB electric field in the spacecraft frame due to orbital motion of the
spacecraft around the Earth as computed from the spacecraft orbital velocity and
measured B-field in the spaceraft frame has been subtracted from the measured
electric field, and so the data product is in the quasi-inertial frame
equivalent to GSE (i.e. it is NOT in the corotation frame of the Earth!).
Each spin fit is time-tagged with the time corresponding to the middle of the
spin of data that went into the spin fit algorithm; in other words, if a given
spin covers the interval [t1, t2), then the spin fit E-field estimate associated
with that spin is given the time tag 0.5*(t1 + t2).
The root mean square residual between the data included in the fit and the
resulting best-fit model, sigma, and the final number of points included in the
spin fit, npts, are also provided at spin-period cadence.
The nominal dynamic range of the E-field estimate is +/- 1 V/m in any component.

• Data Variable Descriptions
  potential [vsvy]

  Single-ended antenna potentials
  

  vsvy_vavg [vsvy_vavg]

  Average of opposing antenna potentials. Units of volts
  

  orbit_num [orbit_num]

  orbit number
  

  Velocity (GSE) [vel_gse]

  Spacecraft velocity in km/s in the GSE coordinate system
  

  Position (GSE) [pos_gse]

  Spacecraft position in GSE coordinates
  

  mlt [mlt]

  Magnetic local time
  

  mlat [mlat]

  magnetic latitude
  

  lshell [lshell]

  lshell from simple dipole model
  

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RBSPB_EFW_BURST-WAVEFORM-UVW-L1 doi:10.48322/zbw6-0626 Copy BibTeX Citation

Description

No TEXT global attribute value.

• Data Variable Descriptions

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RBSPB_L2-1MIN_PSBR-RPS doi:10.48322/r0b5-m046 Copy BibTeX Citation

Description

The RPS instrument is a solid state detector telescope combined with a Cherenkov
radiator. It measures protons with energies from about 60 MeV to about 2 GeV.
For more information, see .http://rbsp.aerospace.org/. For a complete description 
of the instrument, see Mazur et al., 2012, The Relativistic Proton Spectrometer
(RPS) for the Van Allen Probes Mission (formerly known as Radiation Belt Storm
Probes, RBSP), Space Science Reviews. DOI 10.1007/s11214-012-9926-9, 
http://www.springerlink.com/content/p84680786570g7qp/. The instrument PI, Dr.
Joe Mazur, can be reached at Joseph.E.Mazur@aero.org.

Modification History

TBD

• Data Variable Descriptions
  Seconds of livetime in minute [Seconds]
  MET at mid-point of minute [MET_SEC]
  Mission day of level 0 files for this data point [Mission_Day]
  Spacecraft Position (GEO) [Position]
  Position quality flag: 0 - definitive, 1 - predicted [Position_Quality]
  Orbit number [Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [Orbit_Status]
  Decimal hours since perigee [Orbit_Epoch]
  Half-angle of Earth as seen from Spacecraft [EarthConeAngle]
  Measured magnetic field vector in GEO [B_Meas]
  Source of Measured field - 0 indicates MAG L0 file, 1 indicates MAG L1 file, etc. If 255, then the OPQ77 model field is used for computing Alpha and Beta [B_Meas_Flag]
  RPS spin axis vector in GEO vector norm is spin rate [SPIN_OMEGA]
  Counts in data channels based on EVENT_ENERGY_MIN2SSD [DATA_CHANNEL_COUNTS]
  Unidirectional, differential flux vs energy (Isotropic assumption) [FPDI]

  FPDI = Flux Protons Differential Isotropic
  

  RMS error in ln(FPDI) including Poisson and Crosscal Errors [FPDI_RMSE]

  FPDI = Flux Protons Differential Isotropic
  

  Quality flag for FPDI fluxes: 0 - highest quality, 1 - problem with time resolution, 2 - contamination, 3 - saturation, 4 - other problem, 5 - possible electron background, 10 -not yet quality checked [FPDI_Quality]

  FPDI = Flux Protons Differential Isotropic
  

  Mission-Accumulated Dose in Dosimeter 1 (front) [DOSE1]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Dose rate in Dosimeter 1 (front) [DOSE1_RATE]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Mission-Accumulated Dose in Dosimeter 2 (side) [DOSE2]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  Dose rate in Dosimeter 2 (side) [DOSE2_RATE]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  McIlwain L of locally mirroring particle in OPQ [L]

  OPQ
  

  Roederer L of particle with 90 degree pitch angle in OPQ [L_star]

  OPQ
  

  Third (drift) invariant of particle with 90 degree pitch angle in OPQ [Phi]

  OPQ
  

  Equatorial pitch angle of particle with 90 degree pitch angle in OPQ [Alpha_Eq]

  OPQ
  

  OPQ model magnetic field vector in GEO [B_Calc]

  OPQ
  

  OPQ model magnetic field strength at local minimum along local field line [B_Eq]

  OPQ
  

  Magnetic local time (OPQ) [MLT]

  OPQ
  

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RBSPB_L2_PSBR-RPS doi:10.48322/b5me-tj22 Copy BibTeX Citation

Description

The RPS instrument is a solid state detector telescope combined with a Cherenkov
radiator. It measures protons with energies from about 60 MeV to about 2 GeV.
For more information, see .http://rbsp.aerospace.org/. For a complete description 
of the instrument, see Mazur et al., 2012, The Relativistic Proton Spectrometer
(RPS) for the Van Allen Probes Mission (formerly known as Radiation Belt Storm
Probes, RBSP), Space Science Reviews. DOI 10.1007/s11214-012-9926-9, 
http://www.springerlink.com/content/p84680786570g7qp/. The instrument PI, Dr.
Joe Mazur, can be reached at Joseph.E.Mazur@aero.org.

Modification History

TBD

• Data Variable Descriptions
  MET at mid-point of sector [MET_SEC]
  Mission day of level 0 files for this data point [Mission_Day]
  Spacecraft Position (GEO) [Position]
  Position quality flag: 0 - definitive, 1 - predicted [Position_Quality]
  Attitude quality flag: 0 - definitive, 1 - quick-look, 2 - predicted [Attitude_Quality]
  Orbit number [Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [Orbit_Status]
  Decimal hours since perigee [Orbit_Epoch]
  Angle of incidence of particle coming from center of Earth (relative to normal incidence) [EarthRadialAngle]
  Half-angle of Earth as seen from Spacecraft [EarthConeAngle]
  Measured magnetic field vector in GEO [B_Meas]
  Source of Measured field - 0 indicates MAG L0 file, 1 indicates MAG L1 file, etc. If 255, then the OPQ77 model field is used for computing Alpha and Beta [B_Meas_Flag]
  RPS bore sight vector in GEO (parallel to incoming normally incident particle) [BORE_SIGHT]

  Unit vector
  

  RPS spin axis vector in GEO vector norm is spin rate [SPIN_OMEGA]
  Counts in data channels based on EVENT_ENERGY_MIN2SSD [DATA_CHANNEL_COUNTS]
  Unidirectional, differential flux vs energy [FPDU]

  FPDU = Flux Protons Differential Unidirectional
  

  RMS error in ln(FPDU) including Poisson and FPDU_Crosscalib_RMSE [FPDU_RMSE]

  FPDU = Flux Protons Differential Unidirectional
  

  Quality flag for FPDU fluxes: 0 - highest quality, 1 - problem with time resolution (less than 5% live time in sector), 2 - contamination, 3 - saturation, 4 - other problem, 5 - possible electron background, 10 -not yet quality checked [FPDU_Quality]

  FPDU = Flux Protons Differential Unidirectional
  

  Mission-Accumulated Dose in Dosimeter 1 (front) [DOSE1]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Dose rate in Dosimeter 1 (front) [DOSE1_RATE]

  Shielding is about 540 mils Al, DOSE1 on RPS-A did not function correctly.
  

  Mission-Accumulated Dose in Dosimeter 2 (side) [DOSE2]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  Dose rate in Dosimeter 2 (side) [DOSE2_RATE]

  Shielding is about 540 mils Al, DOSE2 did not function correctly on either
  probe.
  

  McIlwain L of locally mirroring particle in OPQ [L90]

  OPQ
  

  Pitch angle of incoming particle along RPS boresight axis [Alpha]
  Gyrophase angle of incoming particle along RPS boresight axis (zero when heading away from Earth) [Beta]
  Spin phase angle of RPS boresight. Phase of 0 occurs at minimum pitch angle. Phase of 90 occurs when Alpha is 90 and increasing [SPIN_PHASE]

  Spin phase 0 occurs at minimum pitch angle. Spin phase90 occures at Alpha=90,
  increasing, and this is the fiducial for defining the spin phase. Spin phase 180
  occurs at maximum pitch angle. Spin phase 270 occurs at Alpha=90, decreasing.
  

  Magnetic field strength at mirror point for incoming particle along RPS boresight axis [B_Mirror]
  Equatorial pitch angle (OPQ) of incoming particle along RPS boresight axis [Alpha_Eq]

  OPQ
  

  McIlwain L of normally incident particle in OPQ [L]

  OPQ
  

  Roederer L of normally incident particle in OPQ [L_star]

  OPQ
  

  Third (drift) invariant of normally incident particle in OPQ [Phi]

  OPQ
  

  McIlwain integral invariant of normally incident particle in OPQ [I]

  OPQ
  

  Kaufmann K, modified second invariant, of normally incident particle in OPQ [K]

  OPQ
  

  OPQ model magnetic field vector in GEO [B_Calc]

  OPQ
  

  OPQ model magnetic field strength at local minimum along local field line [B_Eq]

  OPQ
  

  Magnetic local time (OPQ) [MLT]

  OPQ
  

  Minimum geodetic altitude on drift orbit of normally incident particle in OPQ [h_min]

  OPQ
  

  Equatorial pitch angle (T89Q) of incoming particle along RPS boresight axis [Alpha_Eq_T89Q]
  McIlwain L of normally incident particle in T89Q [L_T89Q]
  Roederer L of normally incident particle in T89Q [L_star_T89Q]
  Third (drift) invariant of normally incident particle in T89Q [Phi_T89Q]
  McIlwain integral invariant of normally incident particle in T89Q [I_T89Q]
  Kaufmann K, modified second invariant, of normally incident particle in T89Q [K_T89Q]
  T89Q model magnetic field vector in GEO [B_Calc_T89Q]
  T89Q model magnetic field strength at local minimum along local field line [B_Eq_T89Q]
  Magnetic local time (T89Q) [MLT_T89Q]
  Minimum geodetic altitude on drift orbit of normally incident particle in T89Q [h_min_T89Q]
  Equatorial pitch angle (T89D) of incoming particle along RPS boresight axis [Alpha_Eq_T89D]
  McIlwain L of normally incident particle in T89D [L_T89D]
  Roederer L of normally incident particle in T89D [L_star_T89D]
  Third (drift) invariant of normally incident particle in T89D [Phi_T89D]
  McIlwain integral invariant of normally incident particle in T89D [I_T89D]
  Kaufmann K, modified second invariant, of normally incident particle in T89D [K_T89D]
  T89D model magnetic field vector in GEO [B_Calc_T89D]
  T89D model magnetic field strength at local minimum along local field line [B_Eq_T89D]
  Magnetic local time (T89D) [MLT_T89D]
  Minimum geodetic altitude on drift orbit of normally incident particle in T89D [h_min_T89D]
  Equatorial pitch angle (TS04D) of incoming particle along RPS boresight axis [Alpha_Eq_TS04D]
  McIlwain L of normally incident particle in TS04D [L_TS04D]
  Roederer L of normally incident particle in TS04D [L_star_TS04D]
  Third (drift) invariant of normally incident particle in TS04D [Phi_TS04D]
  McIlwain integral invariant of normally incident particle in TS04D [I_TS04D]
  Kaufmann K, modified second invariant, of normally incident particle in TS04D [K_TS04D]
  TS04D model magnetic field vector in GEO [B_Calc_TS04D]
  TS04D model magnetic field strength at local minimum along local field line [B_Eq_TS04D]
  Magnetic local time (TS04D) [MLT_TS04D]
  Minimum geodetic altitude on drift orbit of normally incident particle in TS04D [h_min_TS04D]
  MET of event, combination of Packet's MET_SEC and EVENT_SUBTIME_CODE [EVENT_MET]

  Not unique
  

  Mission day of level 0 files for this data point [EVENT_Mission_Day]
  Spacecraft Position (GEO) [EVENT_Position]
  Orbit number [EVENT_Orbit_Number]
  Orbit status: 0 = outbound, 1 = inbound [EVENT_Orbit_Status]
  Decimal hours since perigee [EVENT_Orbit_Epoch]
  McIlwain L of locally mirroring particle in OPQ [EVENT_L90]

  OPQ
  

  McIlwain L of incoming particle along RPS boresight axis [EVENT_L]

  OPQ
  

  Magnetic local time (OPQ) [EVENT_MLT]

  OPQ
  

  Pitch angle of incoming particle along RPS boresight axis [EVENT_Alpha]
  Gyrophase angle of incoming particle along RPS boresight axis (zero when heading away from Earth) [EVENT_Beta]
  Magnetic field strength at mirror point for incoming particle along RPS boresight axis [EVENT_B_Mirror]
  Equatorial pitch angle (OPQ) of incoming particle along RPS boresight axis [EVENT_Alpha_Eq]

  OPQ
  

  D1-D9 detector pulse heights [EVENT_PULSEHEIGHTS]
  D1-D8 Energy Deposit [EVENT_ENERGY_DEPOSIT]
  Coulombs deposited in MCP behind Cherenkov Radiator [EVENT_D9_COULOMBS]
  Photons collected in Cherenkov Radiator [EVENT_CHE_PHOTONS]
  0 - forward, 1 - backward [EVENT_DIRECTION]
  Estimated event energy (uses EVENT_ENERGY_MIN2SSD) [EVENT_ENERGY]
  Estimated event energy using the average of minimum 2 SSD deposits algorithm [EVENT_ENERGY_MIN2SSD]
  Estimated event energy using SSD average algorithm [EVENT_ENERGY_SSDA]
  Estimated event energy using the Cherenkov light only [EVENT_ENERGY_CHE]
  Standard error of ln(EVENT_ENERGY) [EVENT_SIGMA_E]
  ID number of data channel to which the particle is assigned [EVENT_CHANNEL_ID]
  Event classification (-1:INVALID, 0:UNKNOWN, 1:PEN, 2:CHE, 3:ALPHA mode, 127:FILL) [EVENT_TYPE]

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RBSPB_REL03_ECT-MAGEIS-L2 doi:10.48322/mfa4-z841 Copy BibTeX Citation

Description

MagEIS consists of 4 energetic particle sensors per RBSP spacecraft: low unit,
medium35 unit, medium75 unit and the high unit.  The low and 2 medium units are
magnetic spectrometers that measure electrons across roughly the 20 keV - 1 MeV
energy range. The high unit contains a magnetic spectrometer that measures
electrons from roughly the 700 keV to 4 MeV range. The high unit also has a
proton telescope that measures protons from roughly 50 keV to 20 MeV, Helium
ions from roughly 300 keV - 1.5 MeV and Oxygen ions from roughly 1-5 MeV. 
MagEIS is one of three instrument packages on the ECT instrument suite (HOPE and
REPT are the others).

• Data Variable Descriptions
  FESA: Spin-Averaged Differential Electron Flux ~20-4000 keV [FESA]

  Spin-Averaged Differential Electron Flux (FESA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 25 magEIS energy channels. The
  energy channel centroids are specified in FESA_Energy. The channel widths are
  specified in FESA_Energy_Widths. 
  

  ---> FESA as stacked time series [FESA_T]
  ---> % Error in FESA [FESA_ERROR]

  Estimate of the percent error in the uncorrected electron flux.  The percent
  error is defined as a relative error: d(Flux)/Flux, where Flux is the
  uncorrected electron flux.
  

  ---> FESA Quality flag [FESA_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  FESA_CORR: Background-corrected Spin-Averaged Differential Electron Flux ~20-4000 keV [FESA_CORR]

  Spin-Averaged Differential Electron Flux (FESA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 25 magEIS energy channels. The
  energy channel centroids are specified in FESA_Energy. The channel widths are
  specified in FESA_Energy_Widths. 
  

  ---> FESA corrected as stacked time series [FESA_CORR_T]
  ---> % error in FESA corrected [FESA_CORR_ERROR]

  Estimate of the percent error in the background corrected electron flux.  The
  percent error is defined as a relative error: d(Flux)/Flux, where Flux is the
  background corrected electron flux.
  

  FPSA: Spin-Averaged Differential Proton Flux ~50-1500 keV [FPSA]

  Spin-Averaged Differential Proton Flux (FPSA). These data are obtained by
  averaging the sectored fluxes over the data accumulation time (a spin-set,
  nominally equal to 1 spin). Thus, it is not an omni-directional flux, but rather
  a spin-set-averaged flux. Dimension 1 is for the 31 magEIS energy channels. If
  less than 31 channels are used the remaining channel dimensions are set to fill
  values. The energy channel centroids are specified in FPSA_Energy. The channel
  widths are specified in FPSA_Energy_Widths. 
  

  ---> FPSA as stacked time series [FPSA_T]
  ---> % error in FPSA [FPSA_ERROR]

  Estimate of the percent error in the proton flux.  The percent error is defined
  as a relative error: d(Flux)/Flux, where Flux is the proton flux.
  

  ---> FPSA Quality flag [FPSA_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  FPDU: Unidirectional Differential Proton Flux ~50-1500 keV, in up to 31 energy and 64 sector bins (energy-sector displays) [FPDU]

  Unidirectional Differential Proton Flux (FPDU). Dimension 1 is for the 31 magEIS
  energy channels. The energy channel centroids are specified in FPDU_Energy. The
  channel widths are specified in FPDU_Energy_Widths.If less than 31 channels are
  used the remaining channel dimensions are set to fill values. Dimension 2 is for
  the 64 sector angles. Here, the dimension size of 64 is the maximum number of
  possible sectors. If less than 64 are being used, the data are set to fill
  values of -1.0E31. The sector angle values for valid (non-fill) sectors are
  given in FPDU_Sector_Angle.
  

  ---> Spectrograms by sector at sample energies [FPDU_E]
  ---> Spectrograms by energy at sample sectors [FPDU_A]
  ---> [NO PLOTS] % error in FPDU [FPDU_ERROR]

  Estimate of the percent error in the proton flux.  The percent error is defined
  as a relative error: d(Flux)/Flux, where Flux is the proton flux.
  

  ---> [NO PLOTS] FPDU Quality flag [FPDU_Quality]

  Red/Yellow/Green Flag. 2=Red (use data with extreme caution), 1=Yellow (use data
  with caution), 0=Green (no known data issues). 
  
  RED
  1. F less-than dF.  Data is
  set to 0.
  2. dF / F greater-than 1.0 (i.e. F less-than 1.0 * dF).  Low counts,
  large error, or both.
  3. Detector bias is disabled (i.e. in the low-bias
  state).
  4. Livetime less-than 60%.
  
  YELLOW
  1. Background correction was not
  performed. 
  2. dF / F greater-than 0.5 (i.e. F less-than 2.0 * dF).  Low counts,
  large error, or both.
  3. Detector coincidence is disabled (HIGHe only).
  4.
  Livetime correction was not done (main rates and histograms).
  5. There was no
  housekeeping and/or digital status data available (i.e. the test pulser status
  is  unknown, the detector bias status unknown, etc..).
  
  GREEN
  No 'bad' flags
  set. Data is valid to the best of our knowledge.
  

  ---> [NO PLOTS] FPDU Quality flag (Full bitmap) [FPDU_Quality_FULL]

  32-bit flag position. Quality flag is a long int. This is the bit-position that
  is set (from right to left).....0,Background correction was not done (main
  channels).1,The test pulser was on at the current time..2,The detector biases
  were disabled at the current time..3,An engineering look-up-table was used for
  the main and/or derived channel data at the current time. NOTE THAT THE CHANNEL
  MAPPING IS INVALID HERE..4,The front detectors were selected at the current time
  (high unit electron only)..5,The data was set to fill as instructed by the
  calibration file..6,There was no housekeeping and/or digital status data found.
  The bias status, pulser status, etc... is not known..7,There are no main
  channels defined at the current time.8,There are no derived channels defined at
  the current time.9,A validity check failed in the flux conversion. This usually
  indicates that an engineering look-up-table was selected at the current
  time..10,A calibration file could not be found for the current look-up-table ID.
  NOTE THAT THE CHANNEL MAPPING IS INVALID HERE..11,Data was not found at the
  current time for at least one of LOW, MED, HIGH (defined for combined L2 product
  only).12,These channels are not defined for this pixel (HIGH proton only).13,The
  coincidence was disabled at the current time (high unit electron
  only)..14,Livetime correction not applied (main rate): Unknown reason.15,dQ/Q
  greater-than 0.5; Warning. Counts are low and/or error estimate is
  large.16,Livetime correction not applied (histogram): Unknown
  reason.17,Background correction was not done (derived channels).18,The number of
  sectors changed (nsectors)..19,The accumulation interval changed
  (nspins)..20,The LUT changed..21,Livetime correction not applied (main rate):
  The livetime value failed the valid bounds check. This indicates an issue and
  the data is set to fill..22,Livetime correction not applied (main rate):
  pixel-to-channel mapping is invalid.23,Livetime correction not applied (main
  rate): nsectors_main not equal to nsectors_LT.24,Livetime correction not applied
  (main rate): next METs not equal.25,Livetime correction not applied (main rate):
  matching METs not found.26,Livetime correction not applied (main rate): could
  not determine if front or rear detectors were selected (HIGH electron data
  only).27,Livetime correction applied, with warning (main rate): min LT in this
  spin is less than 60%.28,Livetime correction not applied (main rate): no LT
  data.29,dQ/Q greater-than 1.0; Warning. Counts are very low and/or error
  estimate is very large.30,Unit is in sample mode at the given time (i.e.
  background corrections cannot be done)..31,UNUSED
  

  Flag to indicate whether or not the electron coincidence is enabled (0=disabled; 1=enabled). [COINCIDENCE_MODE]

  Flag to indicate whether or not the electron coincidence is enabled (0=disabled;
  1=enabled). This variable is only defined for the HIGH unit (~850-4000 keV), as
  this is the only MagEIS unit with coincidence. In the disabled coincidence
  state, the electron fluxes should only be used qualitatively, and with caution.
  

  ---> Flag to indicate mode of the MagEIS instruments (0=maintenance; 1=science; 2=high rate). [INSTRUMENT_MODE]

  Flag to indicate mode of the MagEIS instruments (0=maintenance; 1=science;
  2=high rate). Only the LOW and MED units (~20-1000 keV) can go into high rate
  mode. The HIGH unit (~850-4000 keV), can only be in maintenance or science mode.
  The most common reason why background corrections cannot be done (e.g.
  FESA_CORR, FEDU_CORR are fill) is when the LOW and/or MED units are in high-rate
  mode.
  

  ---> Flag to indicate whether or not the electron detectors are in the normal-bias or low-bias state (0=low bias; 1=normal bias) [BIAS_MODE]

  Flag to indicate whether or not the electron detectors are in the normal-bias or
  low-bias state (0=low bias; 1=normal bias). In the low-bias state, the electron
  fluxes should only be used qualitatively, and with caution.
  

  ---> Ratio of the background estimate divided by the main rate rate, for the spin-averaged data. [BKG_TO_MAIN_RATIO_SPINAVG]

  Ratio of the background estimate divided by the main rate rate, for the
  spin-averaged data. This gives an estimate of the level of background
  contamination in the main rate data (large % = high background) and/or how close
  the main rate data is to the background level (large % = low counts).
  

  [Time-series] Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates [Position_TT]
  ---> Calculated magnetic field strength [B_Calc_TT]
  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]
  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]
  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]
  ---> Adiabatic invariant (bounce) [I_TT]
  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

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RBSPB_REL03_ECT-REPT-SCI-L2 doi:10.48322/nzhx-1t77 Copy BibTeX Citation

Description

RBSP Relativistic Electron Proton Telescope, Level 2 science data

Modification History

CDF skeleton version of rbsp_rept_science_l2_data.template.cdf written by R.
Reukauf

• Data Variable Descriptions
  Data Quality Flag (0=valid) [Data_Quality]

  0 = valid data; 1 = timing err; 2 = bias_st off; 3 = timing err and bias_st off
  

  FESA: Spin-Averaged Differential Electron Flux 2-20 MeV, in 12 energy bands (spectrogram) [FESA]

  Dimension 1 corresponds to 12 electron energy bins.
  

  ---> (stacked time series) [FESA_E]

  Dimension 1 corresponds to 12 electron energy bins.
  

  FEDU: Unidirectional Differential Electron Flux 2-20 MeV, in 12 energy and 36 angle bins (energy-angle displays) [FEDU]

  Dimension 1 corresponds to 12 electron energy bins.  Dimension 2 holds 36
  sectors.
  

  ---> Spectrograms by energy at sample angles [FEDU_E]
  ---> Spectrograms by angle at sample energies [FEDU_A]

  Dimension 1 corresponds to 12 electron energy bins.  Dimension 2 holds 36
  sectors.
  

  FPSA: Spin-Averaged Differential Proton Flux 20-120 MeV (spectrograms) [FPSA]

  Dimension 1 corresponds to 8 proton energy bins.
  

  ---> (stacked time series) [FPSA_E]

  Dimension 1 corresponds to 8 proton energy bins.
  

  FPDU - Unidirectional Differential Proton Flux 20-120 MeV, in 8 energy and 36 angle bins (energy-angle displays) [FPDU]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  ---> Spectrograms in energy at sample angles [FPDU_E]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  ---> Spectrograms in angle at sample energies [FPDU_A]

  Dimension 1 corresponds to 8 proton energy bins.  Dimension 2 holds 36 sectors.
  

  [Time-series] Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet Calculated with LANLGeomag library. Internal field: IGRF.
  External field: OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates [Position_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength [B_Calc_TT]
  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]
  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]
  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]
  ---> Adiabatic invariant (bounce) [I_TT]
  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

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RBSPB_REL03_ECT-REPT-SCI-L3 doi:10.48322/5t1q-9z75 Copy BibTeX Citation

Description

Van Allen Probes, RBSPECT/REPT (Radiation Belt Storm Probes Energetic particle,
Composition and Thermal plasma suite/Relativistic Electron Proton Telescope,
Level 3 Pitch Angle Sorted Data.

• Data Variable Descriptions
  FEDU - Unidirectional Differential Electron Flux [FEDU]

  Dimension 0 holds 7910 time bins. Dimension 1 corresponds to 17 pitch angle
  bins.  Dimension 2 holds 8 energy bins.
  

  ---> FEDU_byE_atA: Spectrograms by energy at sample pitch angles [FEDU_byE_atA]
  ---> FEDU_byA_atE: Spectrograms by pitch angle at sample energies [FEDU_byA_atE]
  FPDU - Unidirectional Differential Proton Flux [FPDU]

  Dimension 0 holds 7910 time bins. Dimension 1 corresponds to 17 pitch angle
  bins.  Dimension 2 holds 8 energy bins.
  

  ---> FPDU_byE_atA: Spectrograms by energy at sample pitch angles [FPDU_byE_atA]
  ---> FPDU_byA_atE: Spectrograms by pitch angle at sample energies [FPDU_byA_atE]
  FEDU_0to180 - Unidirectional Differential Electron Flux [FEDU_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms at sample pitch angles [FEDU_0to180_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_0to180_byA_atE]
  FEDU_180to360 - Unidirectional Differential Electron Flux [FEDU_180to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_180to360_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FEDU_180to360_byA_atE]
  FPDU_0to180 - Unidirectional Differential Proton Flux [FPDU_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_0to180_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_0to180_byA_atE]
  FPDU_180to360 - Unidirectional Differential Proton Flux [FPDU_180to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 pitch angle bins.
  Dimension 2 holds 8 energy bins.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_180to360_byE_atA]
  ---> Spectrograms by pitch angle at sample energies [FPDU_180to360_byA_atE]
  FEDU_Unbinned_0to180 - Unidirectional Differential Electron Flux (raw sector data). [FEDU_Unbinned_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 12 energy bins.
  

  ---> FEDU_Unbinned_0to360 - Unidirectional Differential Electron Flux (raw sector data). [FEDU_Unbinned_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 12 energy bins.
  

  FPDU_Unbinned_0to180 - Unidirectional Differential Proton Flux (raw sector data). [FPDU_Unbinned_0to180]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 8 energy bins.
  

  ---> FPDU_Unbinned_0to360 - Unidirectional Differential Proton Flux (raw sector data). [FPDU_Unbinned_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins. Dimension 2
  holds 8 energy bins.
  

  [NO PLOTS] FPDU_Unbinned_LightMask_0to360 - LightMask for FPDU_Unbinned_0to360 array. [FPDU_Unbinned_LightMask_0to360]

  Dimensions 0 holds 7910 time bins. Dimension 1 holds 17 sector bins.
  

  ---> FPDU_Unbinned_Light_Flag [FPDU_Unbinned_Light_Flag]

  Dimensions 0 holds 7910 time bins. 
  

  Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT]
  ---> Position in geocentric Geographic coords [Position]
  [TEXT LABELS] Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star_TT]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_TT]

  L-shell parameters are dimensionless. Calculated with LANLGeomag library.
  Internal field: IGRF. External field: OP77Q.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT_TT]

  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT_TT]
  ---> Position - Geocentric position in Re. [Position_TT]

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RBSPB_REL04_ECT-HOPE-MOM-L3 doi:10.48322/ndtr-v928 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by B. Larsen.20140304

• Data Variable Descriptions
  HOPE proton parallel temperature [Tpar_p_30]

  Temperature for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He+ parallel temperature [Tpar_he_30]

  Temperature for he as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE O+ parallel temperature [Tpar_o_30]

  Temperature for o as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE electron parallel temperature [Tpar_e_200]

  Temperature for e as a function of time for apogee mode only from 200 eV energy
  up
  

  HOPE proton perpendicular temperature [Tperp_p_30]

  Temperature for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He+ perpendicular temperature [Tperp_he_30]

  Temperature for he as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE O+ perpendicular temperature [Tperp_o_30]

  Temperature for o as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE electron perpendicular temperature [Tperp_e_200]

  Temperature for e as a function of time for apogee mode only from 200 eV energy
  up
  

  HOPE proton Tperp/Tpar [Tperp_Tpar_p_30]

  Tperp on Tpar for p as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE He Tperp/Tpar [Tperp_Tpar_he_30]

  Tperp on Tpar for he as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE Oxygen Tperp/Tpar [Tperp_Tpar_o_30]

  Tperp over Tpar for o as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE electron Tperp/Tpar [Tperp_Tpar_e_30]

  Tperp over Tpar for e as a function of time for apogee mode only from 30 eV
  energy up
  

  HOPE ion partial density [Ion_density]

  Partial ion density as a function of time for apogee mode only from 30 eV energy
  up
  

  ---> HOPE proton partial density [Dens_p_30]

  Partial density for p as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE He+ partial density [Dens_he_30]

  Partial density for he as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE O+ partial density [Dens_o_30]

  Partial density for o as a function of time for apogee mode only from 30 eV
  energy up
  

  ---> HOPE electron partial density [Dens_e_200]

  Partial density for e as a function of time for apogee mode only from 200 eV
  energy up
  

  HOPE He/p partial density ratio [he_p_ratio]

  Partial density ratio for he/p as a function of time for apogee mode only from
  30 eV energy up
  

  ---> HOPE He/Oxygen partial density ratio [he_o_ratio]

  Partial density ratio for He/O as a function of time for apogee mode only from
  30 eV energy up
  

  ---> HOPE Oxygen/proton partial density ratio [o_p_ratio]

  Partial density ratio for o/p as a function of time for apogee mode only from 30
  eV energy up
  

  Quality Flag for proton temperatures [p_T_flag]

  Flag that is set for suspicious temperature values for p
  

  ---> Quality Flag for He temperatures [he_T_flag]

  Flag that is set for suspicious temperature values for he
  

  ---> Quality Flag for Oxygen temperatures [o_T_flag]

  Flag that is set for suspicious temperature values for o
  

  ---> Quality Flag for electron temperatures [e_T_flag]

  Flag that is set for suspicious temperature values for e
  

  Quality Flag for proton Tperp consistency [p_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for p
  

  ---> Quality Flag for He Tperp consistency [he_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for
  he
  

  ---> Quality Flag for Oxygen Tperp consistency [o_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for o
  

  ---> Quality Flag for electron Tperp consistency [e_Tperp_flag]

  Flag that is set if the two Tperp values are outside 0.5-1.5 of each other for e
  

  Quality Flag for proton density [p_Dens_flag]

  Flag that is set for suspicious density values for p
  

  ---> Quality Flag for He density [he_Dens_flag]

  Flag that is set for suspicious density values for he
  

  ---> Quality Flag for Oxygen density [o_Dens_flag]

  Flag that is set for suspicious density values for o
  

  ---> Quality Flag for electron density [e_Dens_flag]

  Flag that is set for suspicious density values for e
  

  Position of the satellite in geographic coordinates [Position]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Position of the satellite in geographic coordinates [Position_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated Roederers L* parameter (Earths radii) [L_star_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (Earths radii) [L_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated magnetic field strength at magnetic equator [B_Eq_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) [I_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (hours) [MLT_TT]

  Calculated with LANLGeomag library. Internal field: IGRF External field: OP77Q
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

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RBSPB_REL04_ECT-HOPE-PA-L3 doi:10.48322/4671-8e02 Copy BibTeX Citation

Description

Pitch angle binned data from the HOPE plasma spectrometer.  Note that there are
no correections performed on the data (e.g. background subtraction, velocity
corrections, etc.)

Modification History

CDF skeleton version of 20120705. Written by R. Friedel.
20120706 version written by R. Skoug. 
20130715 revisions by J. T. Niehof.
20130808 revisions by J. T. Niehof/BA Larsen.
20130927 revision (remove per-mode variables)by J. T. Niehof.

• Data Variable Descriptions
  FEDO: Omnidirectional differential electron flux ~15-50,000 eV [FEDO]

  Electron flux integrated (piecewise constant) over pitch angle (11) and gyro
  angle (20) as computed from magnetic field direction crossed with spacecraft
  spin axis and energy (72).  Note that data have been expanded to the highest
  possible resolution, even though before 9/2013 the transmitted data are
  collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigee mode excluded) [FEDO_T]

  Electron flux integrated (piecewise constant) over pitch angle (11) and gyro
  angle (20) as computed from magnetic field direction crossed with spacecraft
  spin axis and energy (72).  Note that data have been expanded to the highest
  possible resolution, even though before 9/2013 the transmitted data are
  collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FEDU: Unidirectional Differential Electron Flux ~15-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FEDU]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles (perigee mode excluded) [FEDU_byE_atA]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigee mode excluded) [FEDU_byA_atE]

  Electron flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FPDO: Omnidirectional differential Proton flux ~1-50,000 eV [FPDO]

  Proton flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FPDO_T]

  Proton flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FPDU: Unidirectional Differential Proton Flux ~1-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FPDU]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FPDU_byA_atE]

  Proton flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FODO: Omnidirectional differential Oxygen flux ~1-50,000 eV [FODO]

  Oxygen flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FODO_T]

  Oxygen flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FODU: Unidirectional Differential Oxygen Flux ~1-50,000 eV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FODU]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FODU_byE_atA]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FODU_byA_atE]

  Oxygen flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  FHEDO: Omnidirectional differential Helium flux ~1-50,000 eV [FHEDO]

  Helium flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  ---> (stacked time series; perigees excluded) [FHEDO_T]

  Helium flux integrated (piecewise constant) over pitch angle (11) and gyro angle
  (20) as computed from magnetic field direction crossed with spacecraft spin axis
  and energy (72).  Note that data have been expanded to the highest possible
  resolution, even though before 9/2013 the transmitted data are collapsed (36
  energies, 4-8-16-8-4 spin angles) to fit the telemetry allocation.
  

  FHEDU: Unidirectional Differential Helium Flux ~1-50,000 keV, in 72 energy and 11 pitch angle bins (energy-angle displays) [FHEDU]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by energy at sample pitch angles [FHEDU_byE_atA]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  ---> Spectrograms by pitch angle at sample energies (perigees excluded) [FHEDU_byA_atE]

  Helium flux as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation.
  

  Flags on electron data [Flags_Ele]

  Flags to indicate potential issues with electron data. Each element of this
  array contains the flag status for a particular concern. A flag value of zero
  indicates no unusual concerns of that type for that time sample. Increasing flag
  values indicate increasing concern. See FLAGS variable for a description of each
  element.
  

  ---> Flags on ion data [Flags_Ion]

  Flags to indicate potential issues with electron data. Each element of this
  array contains the flag status for a particular concern. A flag value of zero
  indicates no unusual concerns of that type for that time sample. Increasing flag
  values indicate increasing concern. See FLAGS variable for a description of each
  element.
  

  Mode of electron data [Mode_Ele]

  Indicates instrument mode for electron data. Each mode has a different set of
  energy channels. See corresponding HOPE_ENERGY_Ion record. (0) Apogee mode:
  normal operation. (1) Perigee mode: minimum energy channel raised during pass
  through perigee. (2) burst mode: subset of energies sampled at rapid cadence.
  

  ---> Mode of ion data [Mode_Ion]

  Indicates instrument mode for ion data. Each mode has a different set of energy
  channels. See corresponding HOPE_ENERGY_Ion record. (0) Apogee mode: normal
  operation. (1) Perigee mode: minimum energy channel raised during pass through
  perigee.
  

  HOPE electron counts OMNI [Counts_E_Omni]

  Electron counts summed over pitch angle (11) and gyro angle (20) as computed
  from magnetic field direction crossed with spacecraft spin axis and energy (72).
   Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE electron counts directional [Counts_E]

  Electron counts as a function of pitch angle (11) as computed from magnetic
  field direction crossed with spacecraft spin axis and energy (72).  Note that
  data have been expanded to the highest possible resolution, even though before
  9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles)
  to fit the telemetry allocation. Counts are summed over all measurements in a
  PA/gyro bin.
  

  HOPE proton counts OMNI [Counts_P_Omni]

  Proton counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE proton counts directional [Counts_P]

  Proton counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  HOPE helium counts OMNI [Counts_He_Omni]

  Helium counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE helium counts directional [Counts_He]

  Helium counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  HOPE Oxygen counts OMNI [Counts_O_Omni]

  Oxygen counts summed over pitch angle (11) and gyro angle (20) as computed from
  magnetic field direction crossed with spacecraft spin axis and energy (72). 
  Note that data have been expanded to the highest possible resolution, even
  though before 9/2013 the transmitted data are collapsed (36 energies, 4-8-16-8-4
  spin angles) to fit the telemetry allocation. Counts are summed over all
  measurements in a PA/gyro bin.
  

  ---> [No Plots] HOPE Oxygen counts directional [Counts_O]

  Oxygen counts as a function of pitch angle (11) as computed from magnetic field
  direction crossed with spacecraft spin axis and energy (72).  Note that data
  have been expanded to the highest possible resolution, even though before 9/2013
  the transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit
  the telemetry allocation. Counts are summed over all measurements in a PA/gyro
  bin.
  

  Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  ---> Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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---

RBSPB_REL04_ECT-HOPE-SCI-L2 doi:10.48322/1xw2-1868 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by R. Friedel..20120706 version,
written by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written
by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written by R.
Skoug.20130715 revisions by J. T. Niehof
20120706 version, written by R. Skoug
20130715 revisions by J. T. Niehof

• Data Variable Descriptions
  Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to ion measurement timebase from 1 min. resolution
  MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates(ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  Detector No. [HOPE_DETECTOR]
  Sector No. [HOPE_SECTOR]
  [CreateCDF ONLY] FPDU: Differential directional proton flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FPDU]

  Proton flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FPDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FPDU_D5_BY_ENERGY]
  ---> FPDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FPDU_D5_BY_ANGLE]
  [CreateCDF ONLY] FHeDU: Differential directional helium flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FHEDU]

  Helium flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 3-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FHeDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FHEDU_D5_BY_ENERGY]
  ---> FHeDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FHEDU_D5_BY_ANGLE]
  [CreateCDF ONLY] FODU: Differential directional oxygen flux ~1-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FODU]

  Oxygen flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FODU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FODU_D5_BY_ENERGY]
  ---> FODU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FODU_D5_BY_ANGLE]
  [CreateCDF ONLY] FEDU: Differential directional electron flux ~15-50,000 eV (5 Detectors, 16 Sectors, 72 Energies) [FEDU]

  Electron flux as a function of detector pixel (5), spin angle sector (16), and
  energy (72).  Note that data have been expanded to the highest possible
  resolution (16 spin angles, 72 energies), even though in most cases the
  transmitted data are collapsed (36 energies, 4-8-16-8-4 spin angles) to fit the
  telemetry allocation.
  

  ---> FEDU: Detector 1/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D1_BY_ENERGY]
  -----> Detector 2/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D2_BY_ENERGY]
  -----> Detector 3/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D3_BY_ENERGY]
  -----> Detector 4/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D4_BY_ENERGY]
  -----> Detector 5/Plot: all Energies for the selected sector numbers 1,3,5,7,8,10,12,14,16 [FEDU_D5_BY_ENERGY]
  ---> FEDU: Detector 1/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D1_BY_ANGLE]
  -----> Detector 2/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D2_BY_ANGLE]
  -----> Detector 3/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D3_BY_ANGLE]
  -----> Detector 4/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D4_BY_ANGLE]
  -----> Detector 5/Plot: all Sectors for the selected energy channels 1,9,17,25,33,40,48,56,64,72 [FEDU_D5_BY_ANGLE]

Dataset in CDAWeb
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RBSPB_REL04_ECT-HOPE-SCI-L2SA doi:10.48322/68w5-kh78 Copy BibTeX Citation

Description

none

Modification History

CDF skeleton version of 20120705.Written by R. Friedel..20120706 version,
written by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written
by R. Skoug.20130715 revisions by J. T. Niehof.20120706 version, written by R.
Skoug.20130715 revisions by J. T. Niehof
20120706 version, written by R. Skoug
20130715 revisions by J. T. Niehof

• Data Variable Descriptions
  Position of the satellite in geographic coordinates (ion timebase) [Position_Ion]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to ion measurement timebase from 1 min. resolution
  MagEphem file.
  

  ---> Position of the satellite in geographic coordinates (electron timebase) [Position_Ele]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad. Interpolated to electron measurement timebase from 1 min.
  resolution MagEphem file.
  

  Model magnetic field strength (ion timebase) [B_Calc_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength (electron timebase) [B_Calc_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Model magnetic field strength at magnetic equator (ion timebase) [B_Eq_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Model magnetic field strength at magnetic equator (electron timebase) [B_Eq_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated McIlwains L parameter (ion timebase) [L_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated McIlwains L parameter (electron timebase) [L_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Roederers L* parameter (ion timebase) [L_star_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Roederers L* parameter (electron timebase) [L_star_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Adiabatic invariant (bounce) (ion timebase) [I_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Adiabatic invariant (bounce) (electron timebase) [I_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  Calculated Magnetic Local Time (ion timebase) [MLT_Ion]

  Interpolated to ion measurement timebase from 1 min. resolution MagEphem file.
  Calculated with LANLGeomag library. Internal field: IGRF. External field: OP77Q.
  

  ---> Calculated Magnetic Local Time (electron timebase) [MLT_Ele]

  Interpolated to electron measurement timebase from 1 min. resolution MagEphem
  file. Calculated with LANLGeomag library. Internal field: IGRF. External field:
  OP77Q.
  

  [Labels on plots] Position of the satellite in geographic coordinates(ion) [Position_Ion_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ion) [B_Calc_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator(ion) [B_Eq_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ion) [L_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ion) [L_star_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ion) [I_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ion) [MLT_Ion_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  [Labels on plots] Position of the satellite in geographic coordinates (ele) [Position_Ele_TT]

  Origin = Earths center of mass. X = Intersection of Greenwich meridian and
  geographic equator. Z = Geographic North Pole. Y = completes a right-handed
  Cartesian triad
  

  ---> Calculated magnetic field strength (ele) [B_Calc_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated magnetic field strength at magnetic equator (ele) [B_Eq_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated McIlwains L parameter (Earths radii, ele) [L_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Roederers L* parameter (Earths radii, ele) [L_star_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Adiabatic invariant (bounce, ele) [I_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  ---> Calculated Magnetic Local Time (hours, ele) [MLT_Ele_TT]

  Calculated using ONERA-DESP library Internal field: DGRF/IGRF External field:
  Olson & Pfitzer quiet
  

  Detector No. [HOPE_DETECTOR]
  Sector No. [HOPE_SECTOR]
  HOPE Spin averaged differential oxygen flux (as spectrogram) [FOSA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FOSA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential proton flux [FPSA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FPSA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential helium flux [FHESA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time-series [FHESA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  HOPE Spin averaged differential electron flux [FESA]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

  ---> as stacked time_series [FESA_ts]

  HOPE flux as a function of energy (72), averaged across spin and all detectors.
  Flux from each detector is weighted by the fraction of the unit sphere it
  samples in one spin (9.5% 25% 31% 25% 9.5%). Note that a HOPE spin oversamples
  the spacecraft spin so expect a slight bias depending on the flux in the
  oversampled spin phase for each spin
  

Dataset in CDAWeb
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RBSPB_REL04_ECT-MAGEIS-L3 doi:10.48322/6qrc-aq80 Copy BibTeX Citation

Description

Van Allen Probes, RBSPECT/MagEIS (Radiation Belt Storm Probes Energetic
particle, Composition and Thermal plasma suite/Magnetic Electron Ion
Spectrometer, Level 3 Pitch Angle Sorted Data.

• Data Variable Descriptions
  FEDU: Unidirectional Differential Electron Flux, ~20-4000 keV in 23 energy and 11 pitch angle bins (energy-angle displays) [FEDU_plasmagram]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  [Movie] FEDU: Unidirectional Differential Electron Flux, ~20-4000 keV in 23 energy and 11 pitch angle bins (energy-angle displays) [FEDU_plasmagram_movie]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_byE_atA]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by pitch angle at sample energies [FEDU_byA_atE]

  All FEDU values < Clamp_Threshold_Electron=0.1 are mapped to zero to improve the
  display range.
  

  ---> FEDU_ERROR - sqrt of Unidirectional Differential Electron Counts [FEDU_ERROR]

  Dimension 0 holds 7805 time bins. Dimension 1 corresponds to 11 pitch angle
  bins.  Dimension 2 holds 25 energy bins.
  

  FEDU_CORR - Background-Corrected Unidirectional Differential Electron Flux [FEDU_CORR_plasmagram]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  [Movie] FEDU_CORR - Background-Corrected Unidirectional Differential Electron Flux [FEDU_CORR_plasmagram_movie]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> Spectrograms by energy at sample pitch angles [FEDU_CORR_byE_atA]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> Spectrograms by pitch angle at sample energies [FEDU_CORR_byA_atE]

  All FEDU_CORR values < Clamp_Threshold_Electron=0.1 are mapped to zero to
  improve the display range.
  

  ---> FEDU_CORR_ERROR - Estimate of the percent error in the corrected electron flux. [FEDU_CORR_ERROR]

  Dimension 0 holds 8011 time bins. Dimension 1 corresponds to 11 pitch angle
  bins.  Dimension 2 holds 25 energy bins. The percent error is defined as a
  relative error: d(Flux)/Flux*100%, where Flux is the corrected flux.
  

  FPDU: Unidirectional Differential Proton Flux, ~60-1300 keV in 21 energy and 32 pitch angle bins (energy-angle displays) [FPDU_plasmagram]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  [Movie] FPDU: Unidirectional Differential Proton Flux, ~60-1300 keV in 21 energy and 32 pitch angle bins (energy-angle displays) [FPDU_plasmagram_movie]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by energy at sample pitch angles [FPDU_byE_atA]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  ---> Spectrograms by pitch angle at sample energies [FPDU_byA_atE]

  All FPDU values < Clamp_Threshold_Ion=1.0 are mapped to zero to improve the
  display range.
  

  FDPU_pix1 - Unidirectional Differential Proton Flux [FPDU_pix1]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  ---> [Movie] FDPU_pix1 - Unidirectional Differential Proton Flux [FPDU_pix1_movie]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  FDPU_pix2 - Unidirectional Differential Proton Flux [FPDU_pix2]

  Dimension 0 holds 7918 time bins. Dimension 1 corresponds to 15 pitch angle
  bins.  Dimension 2 holds 31 energy bins.
  

  ---> [Movie] FDPU_pix2 - Unidirectional Differential Proton Flux [FPDU_pix2_movie]

  Dimension 1 corresponds to 15 pitch angle bins.  Dimension 2 holds 31 energy
  bins.
  

  Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star]

  L-shell parameters are dimensionless.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L]

  L-shell parameters are dimensionless.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I]
  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc]
  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq]
  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT]
  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT]
  ---> Position - Geocentric Geocentric position in Re. [Position]
  ---> LstarVsAlpha - Roederer's generalized L-shell parameter. Pitch angle depenedent (pitch angles are local pitch angles). Computed using OP77Q external field and IGRF internal field. [LstarVsAlpha]

  L-shell parameters are dimensionless.
  

  ---> Alpha values for LstarVsAlpha variable. I.e., they are the local pitch angles that L* is computed for in LstarVsAlpha. Units are degrees. [LstarVsAlpha_Alpha]

  Alpha values for LstarVsAlpha variable.
  

  [Labels on plots] Lstar - Roederer's generalized L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_star_TT]

  L-shell parameters are dimensionless.
  

  ---> L - McIlwain's L-shell parameter. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [L_TT]

  L-shell parameters are dimensionless.
  

  ---> I - Integral invariant. Computed for 90deg. particles using OP77Q external field and IGRF internal field. [I_TT]
  ---> B_Calc - Magnitude of computed model field at the S/C. Computed using OP77Q external field and IGRF internal field. [B_Calc_TT]
  ---> B_Eq - Magnitude of computed model field at the Minimum-|B| point along the field line threading the S/C. Computed using OP77Q external field and IGRF internal field. [B_Eq_TT]
  ---> MLT - Eccentric Dipole Magnetic Local Time. Computed using OP77Q external field and IGRF internal field. [MLT_TT]
  ---> MLAT - Eccentric Dipole Magnetic Latitude. Computed using OP77Q external field and IGRF internal field. [MLAT_TT]
  ---> Position - Geocentric Geocentric position in Re. [Position_TT]

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RBSP_ECT-REPT-SCI-L3-SELESNICK-MODEL doi:10.48322/0qyz-h276 Copy BibTeX Citation

Description

The files contain model radiation belt proton intensity derived from data taken
by the Van Allen Probes REPT instruments using the method described by:
Selesnick, R. S., Baker, D. N., Kanekal, S. G., Hoxie, V. C., & Li, X. (2018). 
Modeling the proton radiation belt with Van Allen Probes Relativistic
Electron-Proton Telescope data. Journal of Geophysical Research: Space Physics,
123. https://doi.org/10.1002/2017JA024661 Each file contains average intensity, 
as a function of kinetic energy, equatorial pitch angle, and L-shell, derived
from 1 month of data. 

• Data Variable Descriptions
  Ne kinetic energies [Ne_energies]
  Na equatorial pitch angles [Na_pitchangles]
  L-shells [NL_shells]
  [NO PLOTS] Natural logarithms of NL intensities [intensities]
  Natural Log of Proton Intensity at E=26.1 MeV (#25) [intensities_atE25_byPA_byL]
  ---> Natural Log of Proton Intensity at E=40.9 MeV (#50) [intensities_atE50_byPA_byL]
  ---> Natural Log of Proton Intensity at E=64.0 MeV (#75) [intensities_atE75_byPA_byL]
  ---> Natural Log of Proton Intensity at E=100.1 MeV (#100) [intensities_atE100_byPA_byL]
  ---> Natural Log of Proton Intensity at E=157 MeV (#125) [intensities_atE125_byPA_byL]
  ---> Natural Log of Proton Intensity at E=245 MeV (#150) [intensities_atE150_byPA_byL]
  ---> Natural Log of Proton Intensity at E=383 MeV (#175) [intensities_atE175_byPA_byL]
  Natural Log of Proton Intensity at PA=10.0 deg (#5) [intensities_byE_atPA5_byL]
  ---> Natural Log of Proton Intensity at PA=22.5 deg (#10) [intensities_byE_atPA10_byL]
  ---> Natural Log of Proton Intensity at PA=35.0 deg (#15) [intensities_byE_atPA15_byL]
  ---> Natural Log of Proton Intensity at PA=47.5 deg (#20) [intensities_byE_atPA20_byL]
  ---> Natural Log of Proton Intensity at PA=60.0 deg (#25) [intensities_byE_atPA25_byL]
  ---> Natural Log of Proton Intensity at PA=72.5 deg (#30) [intensities_byE_atPA30_byL]
  ---> Natural Log of Proton Intensity at PA=85.0 deg (#35) [intensities_byE_atPA35_byL]
  Natural Log of Proton Intensity at L=1.35 (#5) [intensities_byE_byPA_atL5]
  ---> Natural Log of Proton Intensity at L=1.6 (#10) [intensities_byE_byPA_atL10]
  ---> Natural Log of Proton Intensity at L=1.85 (#15) [intensities_byE_byPA_atL15]
  ---> Natural Log of Proton Intensity at L=2.1 (#20) [intensities_byE_byPA_atL20]
  ---> Natural Log of Proton Intensity at L=2.35 (#25) [intensities_byE_byPA_atL25]
  ---> Natural Log of Proton Intensity at L=2.6 (#30) [intensities_byE_byPA_atL30]
  ---> Natural Log of Proton Intensity at L=2.85 (#35) [intensities_byE_byPA_atL35]
  ---> Natural Log of Proton Intensity at L=3.1 (#40) [intensities_byE_byPA_atL40]
  ---> Natural Log of Proton Intensity at L=3.35 (#45) [intensities_byE_byPA_atL45]
  [MOVIE DISPLAY] Natural Log of Proton Intensity at E=26.1 MeV (#25) [intensities_movie_atE25_byPA_byL]
  ---> Natural Log of Proton Intensity at E=40.9 MeV (#50) [intensities_movie_atE50_byPA_byL]
  ---> Natural Log of Proton Intensity at E=64.0 MeV (#75) [intensities_movie_atE75_byPA_byL]
  ---> Natural Log of Proton Intensity at E=100.1 MeV (#100) [intensities_movie_atE100_byPA_byL]
  ---> Natural Log of Proton Intensity at E=157 MeV (#125) [intensities_movie_atE125_byPA_byL]
  ---> Natural Log of Proton Intensity at E=245 MeV (#150) [intensities_movie_atE150_byPA_byL]
  ---> Natural Log of Proton Intensity at E=383 MeV (#175) [intensities_movie_atE175_byPA_byL]
  [MOVIE DISPLAY] Natural Log of Proton Intensity at PA=10.0 deg (#5) [intensities_movie_byE_atPA5_byL]
  ---> Natural Log of Proton Intensity at PA=22.5 deg (#10) [intensities_movie_byE_atPA10_byL]
  ---> Natural Log of Proton Intensity at PA=35.0 deg (#15) [intensities_movie_byE_atPA15_byL]
  ---> Natural Log of Proton Intensity at PA=47.5 deg (#20) [intensities_movie_byE_atPA20_byL]
  ---> Natural Log of Proton Intensity at PA=60.0 deg (#25) [intensities_movie_byE_atPA25_byL]
  ---> Natural Log of Proton Intensity at PA=72.5 deg (#30) [intensities_movie_byE_atPA30_byL]
  ---> Natural Log of Proton Intensity at PA=85.0 deg (#35) [intensities_movie_byE_atPA35_byL]
  [MOVIE DISPLAY] Natural Log of Proton Intensity at L=1.35 (#5) [intensities_movie_byE_byPA_atL5]
  ---> Natural Log of Proton Intensity at L=1.6 (#10) [intensities_movie_byE_byPA_atL10]
  ---> Natural Log of Proton Intensity at L=1.85 (#15) [intensities_movie_byE_byPA_atL15]
  ---> Natural Log of Proton Intensity at L=2.1 (#20) [intensities_movie_byE_byPA_atL20]
  ---> Natural Log of Proton Intensity at L=2.35 (#25) [intensities_movie_byE_byPA_atL25]
  ---> Natural Log of Proton Intensity at L=2.6 (#30) [intensities_movie_byE_byPA_atL30]
  ---> Natural Log of Proton Intensity at L=2.85 (#35) [intensities_movie_byE_byPA_atL35]
  ---> Natural Log of Proton Intensity at L=3.1 (#40) [intensities_movie_byE_byPA_atL40]
  ---> Natural Log of Proton Intensity at L=3.35 (#45) [intensities_movie_byE_byPA_atL45]
  [NO PLOTS] 1-sigma uncertainties for the NL natural logarithms of proton intensity [uncertainties]

  These are uncertainties in the natural logarithm of intensity, not in the
  intensity
  

  1-sigma uncertainties for the NL natural logarithms of Proton Intensity at E=40.9 MeV (#50) [uncertainties_atE50_byPA_byL]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at E=100.1 MeV (#100) [uncertainties_atE100_byPA_byL]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at E=245 MeV (#150) [uncertainties_atE150_byPA_byL]
  1-sigma uncertainties for the NL natural logarithms of Proton Intensity at PA=22.5 deg (#10) [uncertainties_byE_atPA10_byL]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at PA=47.5 deg (#20) [uncertainties_byE_atPA20_byL]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at PA=72.5 deg (#30) [uncertainties_byE_atPA30_byL]
  1-sigma uncertainties for the NL natural logarithms of Proton Intensity at L=1.6 (#10) [uncertainties_byE_byPA_atL10]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at L=2.1 (#20) [uncertainties_byE_byPA_atL20]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at L=2.6 (#30) [uncertainties_byE_byPA_atL30]
  ---> 1-sigma uncertainties for the NL natural logarithms of Proton Intensity at L=3.1 (#40) [uncertainties_byE_byPA_atL40]

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REACH-VID-101_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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REACH-VID-102_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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REACH-VID-105_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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REACH-VID-108_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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REACH-VID-113_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-114_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-115_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-116_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-133_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-134_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-135_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-136_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-137_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-138_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-139_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-140_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-148_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-149_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-162_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-163_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-164_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-165_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-166_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  Modified Julian Day [mjd]
  year [year]
  month [month]
  day [day]
  hour [hour]
  minute [minute]
  seconds [seconds]
  Fractional Day of Year [doy]
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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REACH-VID-169_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-170_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-171_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-172_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-173_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-175_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-176_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-180_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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---

REACH-VID-181_DOSIMETER-L1C

Description

The Responsive Environmental Assessment Commercially Hosted (REACH)
constellation is collection of 32 small sensors hosted on six orbital planes of
the Iridium-Next space vehicles in low earth orbit. Each sensor contains two
micro-dosimeters sensitive to the passage of charged particles from the Earth's
radiation belts. There are six distinct dosimeter types spread among the 64
individual sensors, which are unique in shielding and electronic threshold. When
taken together, this effectively enables a high time-cadence measurement of
protons and electrons in six integral energy channels over the entire globe.

• Data Variable Descriptions
  REACH Vehicle Identifier [vid]
  Geodetic Altitude [altitude]
  Geodetic Latitude [latitude]
  Geodetic Longitude [longitude]
  geo_x [geo_x]
  geo_y [geo_y]
  geo_z [geo_z]
  gei_x [gei_x]
  gei_y [gei_y]
  gei_z [gei_z]
  Dose rate from Dosimeter 1 [dose1]
  Proton flux from bowtie [proton_flux1]
  Electron flux from bowtie [electron_flux1]
  Most probable species [species1]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Dose rate from Dosimeter 2 [dose2]
  Proton flux from bowtie [proton_flux2]
  Electron flux from bowtie [electron_flux2]
  Most probable species [species2]

  0 (not currently used); 1-protons, 2-electrons; and 3-both / ambiguous
  

  Housekeeping temperature [hk_temperature]
  Housekeeping voltage 15V [hk_15v_monitor]
  Housekeeping voltage 5V [hk_5v_monitor]
  Housekeeping voltage 3.3V [hk_3_3v_monitor]
  McIlwain L-shell for locally mirroring particle [lm]
  Invariant Latitude for locally mirroring particle [inv_lat]
  Local magnetic field at s/c [blocal]
  Minimum magnetic field on field line intersecting spacecraft [bmin]
  Magnetic local time [mlt]
  k_sqrt [k_sqrt]
  hmin [hmin]
  Local pitch angle [alpha]
  Equatorial pitch angle [alpha_eq]
  region_code [region_code]

  -4: Southern Polar Cap; -3: Outer Zone Untrapped; -2: Slot Untrapped; -1: Inner
  Zone Untrapped; 0: Unknown; 1: Inner Zone Trapped; 2: Slot Trapped; 3: Outer
  Zone Trapped; 4: Northern Polar Cap
  

  orbit_status [orbit_status]

  1=Northbound; 2=Southbound
  

  flag [flag]

  -1: no data; 0: No known problems; 1: Test Mode; 2: Possible temperature-related
  self-counting in Dosimeter A.; 4: Possible temperature-related self-counting in
  Dosimeter B.; 8: Duplicate packets detected.; 16: Unknown issue with VID
  163/Dosimeter B
  

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RENU2_H0_EFIELD doi:10.48322/35v3-c331 Copy BibTeX Citation

Description

RENU2 COrnell Wire BOom Yo-yo (COWBOY)

• Data Variable Descriptions
  electric field - perpendicular East in geomagnetic coordinates, despun with v x B component removed [EpE]
  electric field - perpendicular North in geomagnetic coordinates, despun with v x B component removed [EpN]

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RENU2_H0_EPLAS doi:10.48322/5zvf-1q82 Copy BibTeX Citation

Description

RENU2 EPLAS

• Data Variable Descriptions
  electron energy flux summed over sweep of energies [electron_flux]

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RENU2_H0_ERPAMAIN doi:10.48322/7hy6-k889 Copy BibTeX Citation

Description

RENU2 ERPA

• Data Variable Descriptions
  electron temperature [electron_temperature]
  Peak location (-payload potential) [peak_location]
  Skin Current (density) [skin_current]
  high energy electrons above 3 ev [high_energy_electrons]

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RENU2_H0_ERPASUB doi:10.48322/cy19-2944 Copy BibTeX Citation

Description

RENU2 ERPA

• Data Variable Descriptions
  electron temperature [electron_temperature]
  Peak location (-payload potential) [peak_location]
  Skin Current (density) [skin_current]
  high energy electrons above 3 ev [high_energy_electrons]

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RENU2_H0_FGM doi:10.48322/ndrv-ds51 Copy BibTeX Citation

Description

RENU2 magnetometer

• Data Variable Descriptions
  magnetic field - in geomagneticcoordinates, despun [B]

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RENU2_H0_IG2 doi:10.48322/k3hd-7y51 Copy BibTeX Citation

Description

RENU2 ionization gauge

• Data Variable Descriptions
  sensor_pressure [sensor_pressure]

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RENU2_H0_PMT doi:10.48322/hwz5-q486 Copy BibTeX Citation

Description

RENU2 PMT counts converted to Rayleighs and background subtracted

• Data Variable Descriptions
  Red Line [red_line]
  Green Line [green_line]

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RENU2_H0_UVPMT doi:10.48322/f1c4-b375 Copy BibTeX Citation

Description

RENU2 UV PMT

• Data Variable Descriptions
  counts [counts]

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RENU2_H0_VLF doi:10.48322/7pss-6w70 Copy BibTeX Citation

Description

RENU2 COrnell Wire BOom Yo-yo (COWBOY)

• Data Variable Descriptions
  VLF12 power spectrum [VLF12]
  VLF34 power spectrum [VLF34]

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ROSETTA_HELIO1DAY_POSITION (spase://NASA/NumericalData/Rosetta/HelioWeb/Ephemeris/P1D)

Description

No TEXT global attribute value.

• Data Variable Descriptions
  Distance from Sun to object [RAD_AU]
  Latitude in Solar Ecliptic Coordinate System (SE) [SE_LAT]
  Longitude in Solar Ecliptic Coordinate System (SE) [SE_LON]
  Latitude in heliographic Rotating Coordinate System (HG) [HG_LAT]
  Longitude in Heliographic Rotating Coordinate System (HG) [HG_LON]
  Latitude in heliographic Inertial Coordinate System (HGI) [HGI_LAT]
  Longitude in heliographic Inertial Coordinate System (HGI) [HGI_LON]

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RS_K0_IPEI (spase://NASA/NumericalData/ROCSAT-1/IPEI/PT1s)

Description

1-second averaged data
***Important Notes*** on Accuracy of VperpM_MF (meridional),VperpZ_MF (zonal),
and VparaMF (parallel) components.
Geophysical flow components VperpM_MF, VperpZ_MF, and VparaMF are converted from
flow velocities, Vx, Vy, and Vz 
measured in the S/C coordinate system. Vx points along the S/C trajectory
vector, Vz is in the nadir direction, 
and Vy points to the right of the S/C trajectory vector (in the anti-angular
momentum direction).
1) Vx, Vy, and Vz are measured flow velocities at S/C coordinate in the
Earth-centered Inertia Coordinate System (non-rotating) (ECI coordinate).
2) VperZ_MF, VperM_MF, and VparaMF are geophysical flows in the Earth-centered
Fixed Coordinated System (rotate with the Earth) (ECF coordinate).
3) Uncertainty of +-(37.8-75.45) m/s in Vx based on 0.5% - 1% error in fitting
could be introduced to all geophysical flow components.
4) VperpM_MF at low latitude is almost identical to (-Vz). No Vx is included so
that it is very reliable.
5) Uncertainties from Vx could exist in VperpZ_MF and VparaMF.
6) VperpZ_MF and VparaMF can be used to study the relative changes in flow
velocity due to  geophysical effects.
But can not be used to study the long-term variations because the result could
be biased by the uncertainty in Vx.

Modification History

Version 1.0 Jan. 28, 2008

• Data Variable Descriptions
  Ion drift in S/C LVLH coordinates > x component = along the S/C trajectory vector [vx_rpy]

  Ion drift in S/C LVLH coordinates (in ECI Frame of Reference):   x: along the
  S/C trajectory vector. y: opposite to angular momentum. z: toward the Earth
  Center.
  

  --------------------------> y component = opposite to angular momentum [vy_rpy]

  Ion drift in S/C LVLH coordinates (in ECI Frame of Reference):   x: along the
  S/C trajectory vector. y: opposite to angular momentum. z: toward the Earth
  Center.
  

  --------------------------> z component = toward the Earth Center [vz_rpy]

  Ion drift in S/C LVLH coordinates (in ECI Frame of Reference):   x: along the
  S/C trajectory vector. y: opposite to angular momentum. z: toward the Earth
  Center.
  

  Ion drift in Magnetic Field Coordinates > Component parallel to MF [v1]

  Ion drift in Magnetic Field coordinates (in ECF Frame of Reference) (parallel
  component)
  

  --------------------------> Meridional component perpendicular to MF [v2m]

  Ion drift in Magnetic Field coordinates (in ECF Frame of Reference)
  (perpendicular, meridional component, positive outward(upward)).
  

  --------------------------> Zonal component perpendicular to MF [v2z]

  Ion drift in Magnetic Field coordinates (in ECF Frame of Reference)
  (perpendicular,zonal component, positive eastward).
  

  Total ion density in cm^-3 [Ni]

  Total ion number density in cm^-3
  

  Logarithm (base 10) of total ion density in cm^-3 [logN]

  Logarithm (Base 10) of total ion number density in cm^-3
  

  Ion Temperature (K) [temp]

  Ion Temperature (K)
  

  Ion Composition > percentage of O+ ions [O]

  Ion Composition, percentage of O+ ions
  

  ---------------> percentage of H+ ions [H]

  Ion Composition, percentage of H+ ions
  

  ---------------> percentage of He+ ions [He]

  Ion Composition, percentage of He+ ions
  

  ---------------> percentage of NO+ ions [NO]

  Ion Composition, percentage of NO+ ions
  

  Geographic Latitude [glat]

  Geographic Latitude
  

  Geographic Longitude [glon]

  Geographic Longitude
  

  Dip Latitude [dlat]

  Dip Latitude
  

  Altitude [alt]

  Altitude
  

  Local Time (hr) [lhr]

Dataset in CDAWeb
Data Access Code Examples written in and IDL®.
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