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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-A_WNA-SURVEY_EMFISIS-L4: Probes-A EMFISIS wave normal angle products level Level-4 - Craig Kletzing (University of Iowa)

RBSP-B-RBSPICE_LEV-2_ESRHELT: RBSP_H0_RBSPICE_ESR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_ESRLEHT: RBSP_H0_RBSPICE_ESR_LEHT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_ISRHELT: RBSP_H0_RBSPICE_ISR_HELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_TOFXEH: RBSP_H0_RBSPICE_TOFxE_H - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_TOFXEION: RBSP_H0_RBSPICE_TOFxE_Ion - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_TOFXENONH: RBSP_H0_RBSPICE_TOFxE_nonH - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_TOFXPHHHELT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-2_TOFXPHHLEHT: RBSP_H0_RBSPICE_TOFxPH_H_HELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_ESRHELT: rbsp-b-rbspice_level_3_esrhelt - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_ESRLEHT: rbsp-b-rbspice_level_3_esrleht - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEH: rbsp-b-rbspice_level_3_tofxeh - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEHE-0: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEION: rbsp-b-rbspice_level_3_tofxeion - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXEO-0: rbsp-b-rbspice_level_3_tofxenonh - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHHELT: rbsp-b-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHHLEHT: rbsp-b-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOHELT: rbsp-b-rbspice_level_3_tofxphhhelt - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3-PAP_TOFXPHOLEHT: rbsp-b-rbspice_level_3_tofxphhleht - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_ESRHELT: rbsp-b-rbspice_level_3_ESRHELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_ESRLEHT: rbsp-b-rbspice_level_3_ESRLEHT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_ISRHELT: rbsp-b-rbspice_level_3_ISRHELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_TOFXEH: rbsp-b-rbspice_level_3_TOFXEH - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_TOFXEION: rbsp-b-rbspice_level_3_TOFXEION - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_TOFXENONH: rbsp-b-rbspice_level_3_TOFXENONH - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_TOFXPHHHELT: rbsp-b-rbspice_level_3_TOFXPHHHELT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B-RBSPICE_LEV-3_TOFXPHHLEHT: rbsp-b-rbspice_level_3_TOFXPHHLEHT - Lou Lanzerotti (New Jersey Institute of Technology)

RBSP-B_DENSITY_EMFISIS-L4: Density and other parameters inferred by digitizing the trace on the spectrograms. - Craig Kletzing (University of Iowa)

RBSP-B_HFR-SPECTRA-BURST_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)

RBSP-B_HFR-SPECTRA-MERGED_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)

RBSP-B_HFR-SPECTRA_EMFISIS-L2: Single Axis AC Electric Field Spectra - Craig Kletzing (University of Iowa)

RBSP-B_HFR-WAVEFORM_EMFISIS-L2: High Frequency Receiver Waveform - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_1SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_1SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_1SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_1SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_1SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_4SEC-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_4SEC-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_4SEC-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_4SEC-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_4SEC-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_HIRES-GEI_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_HIRES-GEO_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_HIRES-GSE_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_HIRES-GSM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_HIRES-SM_EMFISIS-L3: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_MAGNETOMETER_UVW_EMFISIS-L2: Fluxgate Magnetometer data - Craig Kletzing (University of Iowa)

RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL-MERGED_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)

RBSP-B_WFR-SPECTRAL-MATRIX-DIAGONAL_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)

RBSP-B_WFR-SPECTRAL-MATRIX_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)

RBSP-B_WFR-WAVEFORM-CONTINUOUS-BURST_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)

RBSP-B_WFR-WAVEFORM_EMFISIS-L2: WFR Spectral Matrix - Craig Kletzing (University of Iowa)

RBSP-B_WNA-SURVEY-SHEATH-CORRECTED-E_EMFISIS-L4: Probes-B EMFISIS wave normal angle products and sheath corrected electric field Level-4 - Craig Kletzing (University of Iowa)

RBSP-B_WNA-SURVEY_EMFISIS-L4: Probes-B EMFISIS wave normal angle products level Level-4 - Craig Kletzing (University of Iowa)

RBSPA_EFW-L2_E-HIRES-UVW: DERIVED FROM: Reference for Spin Axis Vector in GSE - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L2_E-SPINFIT-MGSE: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L2_ESVY_DESPUN: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L2_FBK: Filterbank data product from RBSP-EFW - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L2_SPEC: Spectral data product from RBSP-EFW - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L2_VSVY-HIRES: Single-ended potential values for boom 1-6 - J. R. Wygant (University of Minnesota)

RBSPA_EFW-L3: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPA_EFW_BURST-WAVEFORM-UVW-L1: Burst Mode 1 (512 samples/sec) Electric and Magnetic Fields - J. R. Wygant

RBSPA_L2-1MIN_PSBR-RPS: Van Allen Probes/RPS Level 2 1-Minute Data - J. Mazur (The Aerospace Corporation)

RBSPA_L2_PSBR-RPS: Van Allen Probes/RPS Level 2 Data - J. Mazur (The Aerospace Corporation)

RBSPA_REL03_ECT-MAGEIS-L2: rbsp-a_ect-mageis-l2_pre - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)

RBSPA_REL03_ECT-REPT-SCI-L2: rbspa>Level 2 data for the REPT instrument - D. Baker (University of Colorado at Boulder)

RBSPA_REL03_ECT-REPT-SCI-L3: RBSP/ECT REPT Pitch Angle Resolved Electron and Proton Fluxes. Electron energies: 1.8 - 20 MeV. Proton energies: 21.25 - 4.74961e-316 MeV - D. Baker (University of Colorado at Boulder)

RBSPA_REL04_ECT-HOPE-MOM-L3: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPA_REL04_ECT-HOPE-PA-L3: Pitch angle resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPA_REL04_ECT-HOPE-SCI-L2: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPA_REL04_ECT-HOPE-SCI-L2SA: Spin averaged HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPA_REL04_ECT-MAGEIS-L3: 14 - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)

RBSPB_EFW-L2_E-HIRES-UVW: DERIVED FROM: Reference for Spin Axis Vector in GSE - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L2_E-SPINFIT-MGSE: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L2_ESVY_DESPUN: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L2_FBK: Filterbank data product from RBSP-EFW - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L2_SPEC: Spectral data product from RBSP-EFW - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L2_VSVY-HIRES: Single-ended potential values for boom 1-6 - J. R. Wygant (University of Minnesota)

RBSPB_EFW-L3: DERIVED FROM: Spinfit DC Electric Field estimates in M-GSE coordinates - J. R. Wygant (University of Minnesota)

RBSPB_EFW_BURST-WAVEFORM-UVW-L1: Burst Mode 1 (512 samples/sec) Electric and Magnetic Fields - J. R. Wygant

RBSPB_L2-1MIN_PSBR-RPS: Van Allen Probes/RPS Level 2 1-Minute Data - J. Mazur (The Aerospace Corporation)

RBSPB_L2_PSBR-RPS: Van Allen Probes/RPS Level 2 Data - J. Mazur (The Aerospace Corporation)

RBSPB_REL03_ECT-MAGEIS-L2: rbsp-a_ect-mageis-l2_pre - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)

RBSPB_REL03_ECT-REPT-SCI-L2: rbspb>Level 2 data for the REPT instrument - D. Baker (University of Colorado at Boulder)

RBSPB_REL03_ECT-REPT-SCI-L3: RBSP/ECT REPT Pitch Angle Resolved Electron and Proton Fluxes. Electron energies: 1.8 - 20 MeV. Proton energies: 21.25 - 4.94066e-324 MeV - D. Baker (University of Colorado at Boulder)

RBSPB_REL04_ECT-HOPE-MOM-L3: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPB_REL04_ECT-HOPE-PA-L3: Pitch angle resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPB_REL04_ECT-HOPE-SCI-L2: Spin resolved HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPB_REL04_ECT-HOPE-SCI-L2SA: Spin averaged HOPE science data. Electrons and protons measured in alternate spin cadence. - Herbert Funsten (Los Alamos National Laboratory)

RBSPB_REL04_ECT-MAGEIS-L3: 16 - J. Bernard Blake (JBernard.Blake@aero.org) (The Aerospace Corporation)

RBSP_ECT-REPT-SCI-L3-SELESNICK-MODEL: RBSP/ECT REPT Monthly Intensities as a function of Energy, Pitch Angle and L-shell from the Selesnick model - D. Baker (University of Colorado at Boulder)

REACH-VID-101_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 101 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-102_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 102 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-105_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 105 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-108_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 108 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-113_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 113 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-114_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 114 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-115_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 115 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-116_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 116 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-133_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 133 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-134_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 134 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-135_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 135 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-136_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 136 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-137_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 137 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-138_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 138 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-139_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 139 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-140_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 140 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-148_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 148 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-149_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 149 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-162_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 162 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-163_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 163 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-164_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 164 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-165_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 165 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-166_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 166 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-169_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 169 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-170_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 170 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-171_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 171 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-172_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 172 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-173_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 173 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-175_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 175 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-176_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 176 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-180_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 180 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH-VID-181_DOSIMETER-L1C: Dosimeter measurements from the Responsive Environmental Assessment Commerically Hosted satellite 181 - Joe Mazur (joseph.e.mazur@aero.org) (The Aerospace Corporation)

REACH_ALL_L1C_PRELIM: Preliminary Dosimeter measurements from the Responsive Environmental Assessment Commercially Hosted - 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_HELIO1HR_POSITION: Position in heliocentric coordinates from SPDF Helioweb - Natalia Papitashvili (NASA/GSFC/SPDF)

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

RBSP-A-RBSPICE_LEV-2_ESRHELT doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_ESRLEHT doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_ISRHELT doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_TOFXEH doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_TOFXEION doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_TOFXENONH doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_TOFXPHHHELT doi:tbd
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

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RBSP-A-RBSPICE_LEV-2_TOFXPHHLEHT doi:tbd
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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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RBSP-A_DENSITY_EMFISIS-L4 doi:10.48322/c4ha-xj50

Description

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

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

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.

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

Description

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

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.

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

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.

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RBSP-A_MAGNETOMETER_1SEC-GEI_EMFISIS-L3 doi:10.48322/esgw-y164

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).

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

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).

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RBSP-A_MAGNETOMETER_1SEC-GSE_EMFISIS-L3 doi:10.48322/s5sk-bm30

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).

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RBSP-A_MAGNETOMETER_1SEC-GSM_EMFISIS-L3 doi:10.48322/w6r4-fp76

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).

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

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).

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RBSP-A_MAGNETOMETER_4SEC-GEI_EMFISIS-L3 doi:10.48322/hnyz-nk70

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).

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

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).

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

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).

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RBSP-A_MAGNETOMETER_4SEC-GSM_EMFISIS-L3 doi:10.48322/zrvq-vt55

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).

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

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

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RBSP-A_MAGNETOMETER_HIRES-GEI_EMFISIS-L3 doi:10.48322/q8rs-hg23

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

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RBSP-A_MAGNETOMETER_HIRES-GEO_EMFISIS-L3 doi:10.48322/yhbp-n321

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

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RBSP-A_MAGNETOMETER_HIRES-GSE_EMFISIS-L3 doi:10.48322/hn0a-s943

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

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

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

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RBSP-A_MAGNETOMETER_HIRES-SM_EMFISIS-L3 doi:10.48322/h47r-sf90

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

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

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

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

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

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 doi:10.48322/be1v-n754

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

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

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-A_WNA-SURVEY_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).
 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!dparallel!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 along axis2 (eastward).

COHERENCE BETWEEN B!dperp1!n AND B!dperp2!n [cohb1_2]

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).

COHERENCE BETWEEN B!dperp1!n AND B!dpar!n [cohb1_3]

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).

COHERENCE BETWEEN B!dperp2!n AND B!dpar!n [cohb2_3]

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).

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.

POWER SPECTRAL DENSITY OF E!dparallel!n [e3]

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

DEGREE OF POLARIZATION OF THE MAGNETIC FIELD FROM EIGENVALUES [eigen]

Eigenvalues are determined using the SVD method

ELLIPTICITY OF THE MAGNETIC FIELD POLARIZATION [ellsvd]

Determined using the SVD method, from equation 13 of Santolik et al, 2003

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).

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.

AZIMUTHAL ANGLE OF THE WAVE VECTOR [phsvd]

Wave Normal Angles are determined using the SVD method

PLANARITY OF THE MAGNETIC FIELD POLARIZATION [plansvd]

Determined using the SVD method, from equation 12 of Santolik et al, 2003

ELECTROMAGNETIC PLANARITY [plansvde]

Electromagnetic planarity calculated from the 6x6 spectral matrix using eq. 24
of  Santolik, O., M. Parrot, and F. Lefeuvre, Singular value decomposition
methods for wave propagation analysis, Radio. Sci. 38(1), 1010,
doi:10.1029/2000RS002523, 2003.

DEGREE OF MAGNETIC FIELD POLARIZATION IN THE POLARIZATION PLANE [polsvd]

Determined using the SVD method, from equation (A6) in the appendix of Santolik
et al, 2002

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.

POLAR ANGLE OF THE WAVE VECTOR [thsvd]

Wave Normal Angles are determined using the SVD method

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).

Radial distance, Re [R]

Magnetic Latitude, Deg [MagLat]

Magnetic Local Time, Hrs [MLT]

L Shell [L]

Transformation Matrix, UVW->Field-Aligned Coordinates [Tuvw2fac]

If V is a vector field value in the antenna frame [u, v, w], then Tuvw2fac ## V
is that same quantity in the field-aligned coordinate system, with axis3 along
B0, axis1 outward from the Earth, and axis2 eastward

Buvw, nT [Buvw]

The 3-vector B field from the EMFISIS MAG instrument in the spacecraft antenna
coordinate system, with axis3 (w) along the spin-axis, axis1 (u) and axis2 (v)
in the spin plane. Value is a linear interpolation between the two nearest (in
time) magnetometer measurements to the specific epochs in this CDF.

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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RBSP-B-RBSPICE_LEV-3_ESRLEHT doi:10.48322/nxsw-2k50

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

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

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

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

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

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RBSP-B-RBSPICE_LEV-3_TOFXEION doi:10.48322/1qnv-8c11

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

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RBSP-B-RBSPICE_LEV-3_TOFXENONH doi:10.48322/w7nq-kz93

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

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RBSP-B-RBSPICE_LEV-3_TOFXPHHHELT doi:10.48322/6wj8-zz20

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

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

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

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RBSP-B_DENSITY_EMFISIS-L4 doi:10.48322/c6s1-wg66

Description

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

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

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.

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

Description

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RBSP-B_HFR-SPECTRA_EMFISIS-L2 doi:10.48322/zpmq-qm18

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.

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RBSP-B_HFR-WAVEFORM_EMFISIS-L2 doi:10.48322/dz64-x875

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.

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

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).

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

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).

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

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).

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RBSP-B_MAGNETOMETER_1SEC-GSM_EMFISIS-L3 doi:10.48322/x429-5310

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).

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RBSP-B_MAGNETOMETER_1SEC-SM_EMFISIS-L3 doi:10.48322/fg6n-yr78

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).

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

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).

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

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).

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RBSP-B_MAGNETOMETER_4SEC-GSE_EMFISIS-L3 doi:10.48322/e698-nb28

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).

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RBSP-B_MAGNETOMETER_4SEC-GSM_EMFISIS-L3 doi:10.48322/kh8k-hc54

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

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RBSP-B_MAGNETOMETER_4SEC-SM_EMFISIS-L3 doi:10.48322/knn2-mp16

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

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RBSP-B_MAGNETOMETER_HIRES-GEI_EMFISIS-L3 doi:10.48322/b30v-s029

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

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RBSP-B_MAGNETOMETER_HIRES-GEO_EMFISIS-L3 doi:10.48322/y09z-a990

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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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RBSP-B_WNA-SURVEY_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).
 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!dparallel!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 along axis2 (eastward).

COHERENCE BETWEEN B!dperp1!n AND B!dperp2!n [cohb1_2]

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).

COHERENCE BETWEEN B!dperp1!n AND B!dpar!n [cohb1_3]

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).

COHERENCE BETWEEN B!dperp2!n AND B!dpar!n [cohb2_3]

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).

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.

POWER SPECTRAL DENSITY OF E!dparallel!n [e3]

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

DEGREE OF POLARIZATION OF THE MAGNETIC FIELD FROM EIGENVALUES [eigen]

Eigenvalues are determined using the SVD method

ELLIPTICITY OF THE MAGNETIC FIELD POLARIZATION [ellsvd]

Determined using the SVD method, from equation 13 of Santolik et al, 2003

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).

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).

AZIMUTHAL ANGLE OF THE WAVE VECTOR [phsvd]

Wave Normal Angles are determined using the SVD method

PLANARITY OF THE MAGNETIC FIELD POLARIZATION [plansvd]

Determined using the SVD method, from equation 12 of Santolik et al, 2003

ELECTROMAGNETIC PLANARITY [plansvde]

Electromagnetic planarity calculated from the 6x6 spectral matrix using eq. 24
of  Santolik, O., M. Parrot, and F. Lefeuvre, Singular value decomposition
methods for wave propagation analysis, Radio. Sci. 38(1), 1010,
doi:10.1029/2000RS002523, 2003.

DEGREE OF MAGNETIC FIELD POLARIZATION IN THE POLARIZATION PLANE [polsvd]

Determined using the SVD method, from equation (A6) in the appendix of Santolik
et al, 2002

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.

POLAR ANGLE OF THE WAVE VECTOR [thsvd]

Wave Normal Angles are determined using the SVD method

Radial distance, Re [R]

Magnetic Latitude, Deg [MagLat]

Magnetic Local Time, Hrs [MLT]

L Shell [L]

Transformation Matrix, UVW->Field-Aligned Coordinates [Tuvw2fac]

If V is a vector field value in the antenna frame [u, v, w], then Tuvw2fac ## V
is that same quantity in the field-aligned coordinate system, with axis3 along
B0, axis1 outward from the Earth, and axis2 eastward

Buvw, nT [Buvw]

The 3-vector B field from the EMFISIS MAG instrument in the spacecraft antenna
coordinate system, with axis3 (w) along the spin-axis, axis1 (u) and axis2 (v)
in the spin plane. Value is a linear interpolation between the two nearest (in
time) magnetometer measurements to the specific epochs in this CDF.

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RBSPA_EFW-L2_E-HIRES-UVW doi:10.48322/qtvb-dd97

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

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

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

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

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RBSPA_EFW-L2_SPEC doi:10.48322/78pf-4k59

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

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RBSPA_EFW-L2_VSVY-HIRES doi:10.48322/7mwt-de58

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-L3 doi:10.48322/4k9n-gs06

Description

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

Corotation Efield(MGSE) [VxB_efield_of_earth_mgse]

Corotation efield equals to Omega x R x B in the MGSE coordinate system, where B
is measured magnetic field, Omega is the Earth's spin axis angular frequency
vector, and R is the vector from the Earth's center to the satellite

Einertial(12,MGSE) spinfit [efield_in_inertial_frame_spinfit_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted)
derived from the EFW e12 (V1-V2) data product.

Ecoro(12,MGSE) spinfit [efield_in_corotation_frame_spinfit_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted,
corotation Efield subtracted) derived from the EFW e12 (V1-V2) data product.
Corotation Efield calculated from Omega x R x B in MGSE coord. Omega is the
Earth's spin axis vector and R is the vector from the Earth's center to the
satellite

Einertial(12,MGSE) spinfit [efield_in_inertial_frame_spinfit_edotb_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted)
derived from the EFW e12 (V1-V2) data product. Spin axis component derived from
E*B=0.

Ecoro(12,MGSE) spinfit [efield_in_corotation_frame_spinfit_edotb_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted,
corotation Efield subtracted) derived from the EFW e12 (V1-V2) data product.
Corotation Efield calculated from Omega x R x B in MGSE coord. Omega is the
Earth's spin axis vector and R is the vector from the Earth's center to the
satellite

spacecraft potential(12) [spacecraft_potential]

Average of opposing antenna potentials (V1+V2)/2.

density(12) [density]

Density estimation from sc potential, determined from the form density =
A1*exp(b*x)+A2*exp(c*x), where x=(V1 + V2)/2, where the constants are found by
comparison to upper hybrid line from EMFISIS. The fit is updated approximately
monthly. For a more accurate density (or verification) for a specific time
period contact the EFW team. Values below 10cm-3 and above 3000 cm-3 are
untrustworthy and are removed

Vsc x B (MGSE) [VscxB_motional_efield_mgse]

Electric field equals to Vsc x B in the MGSE coordinate system, where Vsc is
spacecraft velocity and B is the measured magnetic field

Velocity (GSE) [velocity_gse]

Spacecraft velocity in km/s in the GSE coordinate system

Position (GSE) [position_gse]

Spacecraft position in km in the GSE coordinate system

angle_spinplane_Bo [angle_spinplane_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. The RBSP spinaxis
pointing direction determined from SPICE

mlt [mlt]

Spacecraft magnetic local time in hour

mlat [mlat]

Spacecraft magnetic latitude in deg

lshell [lshell]

Spacecraft L-shell from simple dipole model

L_vector [spinaxis_gse]

Unit vector of spin axis (w) in the GSE coordinate system, also the pointing
direction defining the spacecraft angular velocity

Global flag [global_flag]

Global Flag

---> EFW Global Data Quality [flag_global]

EFW flag values(12) [flags_all]

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.

bias_current [bias_current]

Bias current (nA) applied to the antenna probes

flags_charging_bias_eclipse [flags_charging_bias_eclipse]

charging, bias, eclipse flags, extreme charging

burst1_avail [burst1_avail]

Burst 1 data availability flag

burst2_avail [burst2_avail]

Burst 2 data availability flag

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RBSPA_EFW_BURST-WAVEFORM-UVW-L1 doi:10.48322/jcd5-kf50

Description

No TEXT global attribute value.

Data Variable Descriptions

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

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

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RBSPA_L2_PSBR-RPS doi:10.48322/a587-0r70

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

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RBSPA_REL03_ECT-MAGEIS-L2 doi:10.48322/dhj8-f337

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

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

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

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RBSPA_REL04_ECT-HOPE-MOM-L3 doi:10.48322/egeg-7005

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

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

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RBSPA_REL04_ECT-HOPE-SCI-L2 doi:10.48322/34q8-8q26

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

Dataset in CDAWeb
Data Access Code Examples written in

and IDL®.
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RBSPA_REL04_ECT-HOPE-SCI-L2SA doi:10.48322/rcxw-mm23

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

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

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RBSPB_EFW-L2_E-HIRES-UVW doi:10.48322/64bn-y776

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

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

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

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

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RBSPB_EFW-L2_SPEC doi:10.48322/hdnm-mh60

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

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RBSPB_EFW-L2_VSVY-HIRES doi:10.48322/e9bt-8x09

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-L3 doi:10.48322/p4ze-4247

Description

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

Corotation Efield(MGSE) [VxB_efield_of_earth_mgse]

Corotation efield equals to Omega x R x B in the MGSE coordinate system, where B
is measured magnetic field, Omega is the Earth's spin axis angular frequency
vector, and R is the vector from the Earth's center to the satellite

Einertial(12,MGSE) spinfit [efield_in_inertial_frame_spinfit_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted)
derived from the EFW e12 (V1-V2) data product.

Ecoro(12,MGSE) spinfit [efield_in_corotation_frame_spinfit_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted,
corotation Efield subtracted) derived from the EFW e12 (V1-V2) data product.
Corotation Efield calculated from Omega x R x B in MGSE coord. Omega is the
Earth's spin axis vector and R is the vector from the Earth's center to the
satellite

Einertial(12,MGSE) spinfit [efield_in_inertial_frame_spinfit_edotb_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted)
derived from the EFW e12 (V1-V2) data product. Spin axis component derived from
E*B=0.

Ecoro(12,MGSE) spinfit [efield_in_corotation_frame_spinfit_edotb_mgse]

Spin-fit electric field in the MGSE coordinate system (Vsc x B subtracted,
corotation Efield subtracted) derived from the EFW e12 (V1-V2) data product.
Corotation Efield calculated from Omega x R x B in MGSE coord. Omega is the
Earth's spin axis vector and R is the vector from the Earth's center to the
satellite

spacecraft potential(12) [spacecraft_potential]

Average of opposing antenna potentials (V1+V2)/2.

density(12) [density]

Density estimation from sc potential, determined from the form density =
A1*exp(b*x)+A2*exp(c*x), where x=(V1 + V2)/2, where the constants are found by
comparison to upper hybrid line from EMFISIS. The fit is updated approximately
monthly. For a more accurate density (or verification) for a specific time
period contact the EFW team. Values below 10cm-3 and above 3000 cm-3 are
untrustworthy and are removed

Vsc x B (MGSE) [VscxB_motional_efield_mgse]

Electric field equals to Vsc x B in the MGSE coordinate system, where Vsc is
spacecraft velocity and B is the measured magnetic field

Velocity (GSE) [velocity_gse]

Spacecraft velocity in km/s in the GSE coordinate system

Position (GSE) [position_gse]

Spacecraft position in km in the GSE coordinate system

angle_spinplane_Bo [angle_spinplane_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. The RBSP spinaxis
pointing direction determined from SPICE

mlt [mlt]

Spacecraft magnetic local time in hour

mlat [mlat]

Spacecraft magnetic latitude in deg

lshell [lshell]

Spacecraft L-shell from simple dipole model

L_vector [spinaxis_gse]

Unit vector of spin axis (w) in the GSE coordinate system, also the pointing
direction defining the spacecraft angular velocity

Global flag [global_flag]

Global Flag

---> EFW Global Data Quality [flag_global]

EFW flag values(12) [flags_all]

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.

bias_current [bias_current]

Bias current (nA) applied to the antenna probes

flags_charging_bias_eclipse [flags_charging_bias_eclipse]

charging, bias, eclipse flags, extreme charging

burst1_avail [burst1_avail]

Burst 1 data availability flag

burst2_avail [burst2_avail]

Burst 2 data availability flag

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RBSPB_EFW_BURST-WAVEFORM-UVW-L1 doi:10.48322/zbw6-0626

Description

No TEXT global attribute value.

Data Variable Descriptions

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RBSPB_L2-1MIN_PSBR-RPS doi:10.48322/r0b5-m046

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

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RBSPB_L2_PSBR-RPS doi:10.48322/b5me-tj22

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

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RBSPB_REL03_ECT-MAGEIS-L2 doi:10.48322/mfa4-z841

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

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

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

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RBSPB_REL04_ECT-HOPE-MOM-L3 doi:10.48322/ndtr-v928

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

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

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RBSPB_REL04_ECT-HOPE-SCI-L2 doi:10.48322/1xw2-1868

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

Dataset in CDAWeb
Data Access Code Examples written in

and IDL®.
Back to top

RBSPB_REL04_ECT-HOPE-SCI-L2SA doi:10.48322/68w5-kh78

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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RBSPB_REL04_ECT-MAGEIS-L3 doi:10.48322/6qrc-aq80

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.

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RBSP_ECT-REPT-SCI-L3-SELESNICK-MODEL doi:10.48322/0qyz-h276

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.

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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

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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

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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

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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.

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

Dataset in CDAWeb
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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

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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

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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

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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

Dataset in CDAWeb
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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

Dataset in CDAWeb
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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

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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

Dataset in CDAWeb
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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

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REACH_ALL_L1C_PRELIM doi:10.5281/zenodo.5988170
Proper citations should include the "Accessed on date" in the form .

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.

Modification History

v1.0.0 - Original version.

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RENU2_H0_EFIELD doi:10.48322/35v3-c331

Description

RENU2 COrnell Wire BOom Yo-yo (COWBOY)

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RENU2_H0_EPLAS doi:10.48322/5zvf-1q82

Description

RENU2 EPLAS

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RENU2_H0_ERPAMAIN doi:10.48322/7hy6-k889

Description

RENU2 ERPA

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RENU2_H0_ERPASUB doi:10.48322/cy19-2944

Description

RENU2 ERPA

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RENU2_H0_FGM doi:10.48322/ndrv-ds51

Description

RENU2 magnetometer

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RENU2_H0_IG2 doi:10.48322/k3hd-7y51

Description

RENU2 ionization gauge

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RENU2_H0_PMT doi:10.48322/hwz5-q486

Description

RENU2 PMT counts converted to Rayleighs and background subtracted

Data Variable Descriptions

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RENU2_H0_UVPMT doi:10.48322/f1c4-b375

Description

RENU2 UV PMT

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RENU2_H0_VLF doi:10.48322/7pss-6w70

Description

RENU2 COrnell Wire BOom Yo-yo (COWBOY)

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ROSETTA_HELIO1HR_POSITION

Description

No TEXT global attribute value.

Data Variable Descriptions

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RS_K0_IPEI doi:10.48322/jz5h-kr21

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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