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1) GOES 1 Energetic Particle Monitor at 3 sec Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/1/EPM/PT3S
Start:1976-01-01 00:00:00 Observatory:GOES 1 Cadence:3 seconds
Stop:1978-05-31 00:00:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 1 EPM data set contains various parameters at 3 s resolution. Within the data files is the time given as seconds of the month where the date is given in the filename, a flag word that provides information on the data and satellite command state in a flagword, and the measured counts for a subset of available channels, which are indicated by the flagword.

2) GOES 1 Magnetic Field Monitor at 3 sec Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/1/MFM/PT3S
Start:1976-01-01 00:00:00 Observatory:GOES 1 Cadence:3 seconds
Stop:1978-05-31 00:00:00 Instrument:Biaxial Fluxgate Magnetometer Resource:NumericalData
A biaxial, closed-loop, fluxgate magnetometer was deployed on a boom about 0.61 m long. The magnetometer, which had one sensor aligned parallel to the spacecraft spin axis and the other perpendicular to this axis, measured the magnetic field at synchronous altitude. Each sensor had a selectable range (+50, 100, 200, or 400 nT), an offset field capability (plus or minus 1200 nT in 40-nT steps), and an inflight calibration capability.

3) GOES 10 High Energy Proton and Alpha Detector (HEPAD) data at 5 m Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/HEPAD/PT5M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 23:59:59 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
The GOES 10 High Energy Proton and Alpha Detector (HEPAD) provides flux measurements of high energy proton and alpha particles. This data set consists of protons in 4 energy channels from 350 to >700 MeV and the alpha particles consist of 2 energy channels from 2560 to >3400 MeV.

4) GOES 10 high-resolution magnetometer data maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/MAG/PT0.512S
Start:2006-12-31 23:59:58 Observatory:GOES 10 Cadence:0.512 seconds
Stop:2008-12-31 23:59:58 Instrument:GOES 10, Triaxial Fluxgate Magnetometer Resource:NumericalData
GOES 10 magnetic field data at 0.512 second time resolution. The vector magnetic field is given in the spacecraft (s/c) earth-referenced coordinate system: Hp, He, Hn, and Ht, where Hp is perpendicular to the satellite orbital plane, or parallel to Earth's spin axis in the case of a zero degree inclination orbit; He is perpendicular to Hp and directed earthwards; Hn is perpendicular to both Hp and He and directed eastwards; and Ht is the total field. This data product also provides GOES 10 satellite positions and velocities derived from SSCWEB GEI ephemeris, interpolated to one minute time resolution. The magnetometer data are downlinked from the spacecraft in real-time to the NOAA Space Weather Prediction Center (SWPC) in Boulder, CO. The data from the raw Command and Data Acquisition (CDA) telemetry stream are processed by pre-processors at SWPC and from there 1-minute averages are distributed to SWPC Space Weather Operations, as well a archived at NOAA?s National Geophysical Data Center (NGDC) and NASA?s Coordinated Data Analysis Web (http://cdaweb.gsfc.nasa.gov/). The raw high-resolution data are corrected and processed at NOAA?s SWPC, and later archived at NGDC. The major issue for processing the high-resolution data is correction for the magnetic signature of spacecraft torquer currents as briefly discussed in the magnetometer instrument descriptions. In normal operation, the magnetometer samples its three axes every 0.512 seconds, synchronized with the telemetry frames. The magnetometer has an anti-aliasing low-pass filter on each axis. As part of the attitude control on the spacecraft, there are two magnetic torquers. At the magnetometers, these torquers can generate magnetic fields larger than the ambient fields to be measured. Therefore signals from these torquer currents need to be removed. The torquer currents are measured at the same rate as the magnetometer rate, and the currents are used to correct the magnetometer measurements. However, the torquer currents were not low-pass filtered. As a result, large instantaneous steps in the torquer currents show up in the magnetometer data as a delayed, slowly rising wave with some ringing, just what one would expect from the magnetometer low-pass filters. The so-called ?Farthing coefficients? simulate, from a short past history of the torquer measurements, the effects of the magnetometer filters. The torquer current changes are asynchronous with the telemetry frames and the timing between these events must be measured to a eighth of a telemetry frame interval for good performance. The transient responses in changes in torquer currents are reduced, but not eliminated for large changes in torquer currents. There exists one opportunity at the beginning of each mission to perform a spacecraft rotation maneuver to determine magnetometer offsets. These offsets are used through the duration of each satellite's lifetime. Approximate coefficients are: * 0.8 milliampere per torquer current count * 4 counts per torquer current command step (3.2 milliampere per command step) * 410 milliamperes full scale current * 32 magnetometer counts per nT (approximate) * 8 torquer step counts can be up to approximately 0.5 nT (depends on axis, which torquer, which satellite, etc.)

5) GOES 10 Magnetometer 1-Minute Data maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/MAG/PT1M
Start:1999-03-21 00:00:30 Observatory:GOES 10 Cadence:1 minute
Stop:2006-06-22 23:59:30 Instrument:GOES 10, Triaxial Fluxgate Magnetometer Resource:NumericalData
The NOAA Geostationary Operational Environment Satellite (GOES) key parameters. This data is a subset of the data available from the GOES Space Environment Monitor (SEM) instruments. It contains vector magnetic field in three coordinate systems: * (1) Spacecraft P,E,N * (2) GSM x,y,z and * (3) GSE x,y,z. Spacecraft magnetic field is defined as: * P - perpendicular to the spacecraft orbital plane or parallel to the Earth's spin axis in the case of a zero degree inclination orbit; * E - perpendicular to P and directed earhtwards; and * N - perpendicular to both P and E and directed eastwards.

6) GOES 10 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/A/PT5M
Start:1998-08-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected alpha-particle fluxes for several energy ranges.

7) GOES 10 Space Evironment Monitor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/G/PT1M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:1 minute
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 1 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

8) GOES 10 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/G/PT5M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

9) GOES 10 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/H/PT5M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton and alpha particle fluxes for several energy ranges.

10) GOES 10 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/I/PT5M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

11) GOES 10 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/SEM/Z/PT5M
Start:1998-07-01 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 10 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

12) GOES 11 Energetic Particle Sensor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/EPS/PT1M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:1 minute
Stop:2011-02-28 23:59:59 Instrument:Environment Monitor Resource:NumericalData
The energetic particle sensor data consists of electron and proton data. The electrons consists of 3 energy flux channels with energies greater than 0.6 MeV. The proton fluxes consist of 7 energy channels from 0.6 to 500 MeV.

13) GOES 11 Energetic Particle Sensor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/EPS/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2011-02-28 23:59:59 Instrument:Environment Monitor Resource:NumericalData
The energetic particle sensor data consists of electron, proton, and alpha particle data. The electrons consists of 3 energy flux channels with energies greater than 0.6 MeV. The protons consist of 7 energy channels from 0.6 to 500 MeV and the alpha particles consist of 6 energy channels from 4 to 500 MeV.

14) GOES 11 High Energy Proton and Alpha Detector (HEPAD) data at 5 m Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/HEPAD/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2011-02-28 23:59:59 Instrument:Environment Monitor Resource:NumericalData
The GOES 11 High Energy Proton and Alpha Detector (HEPAD) provides flux measurements of high energy proton and alpha particles. This data set consists of protons in 4 energy channels from 350 to >700 MeV and the alpha particles consist of 2 energy channels from 2560 to >3400 MeV.

15) GOES 11 high-resolution magnetometer data maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/MAG/PT0.512S
Start:2007-09-15 23:59:58 Observatory:GOES 11 Cadence:0.512 seconds
Stop:2008-06-30 23:59:58 Instrument:GOES 11, Triaxial Fluxgate Magnetometer Resource:NumericalData
GOES 11 magnetic field data at 0.512 second time resolution. The vector magnetic field is given in the spacecraft (s/c) earth-referenced coordinate system: Hp, He, Hn, and Ht, where Hp is perpendicular to the satellite orbital plane, or parallel to Earth's spin axis in the case of a zero degree inclination orbit; He is perpendicular to Hp and directed earthwards; Hn is perpendicular to both Hp and He and directed eastwards; and Ht is the total field. This data product also provides GOES 11 satellite positions and velocities derived from SSCWEB GEI ephemeris, interpolated to one minute time resolution. The magnetometer data are downlinked from the spacecraft in real-time to the NOAA Space Weather Prediction Center (SWPC) in Boulder, CO. The data from the raw Command and Data Acquisition (CDA) telemetry stream are processed by pre-processors at SWPC and from there 1-minute averages are distributed to SWPC Space Weather Operations, as well a archived at NOAA?s National Geophysical Data Center (NGDC) and NASA?s Coordinated Data Analysis Web (http://cdaweb.gsfc.nasa.gov/). The raw high-resolution data are corrected and processed at NOAA?s SWPC, and later archived at NGDC. The major issue for processing the high-resolution data is correction for the magnetic signature of spacecraft torquer currents as briefly discussed in the magnetometer instrument descriptions. In normal operation, the magnetometer samples its three axes every 0.512 seconds, synchronized with the telemetry frames. The magnetometer has an anti-aliasing low-pass filter on each axis. As part of the attitude control on the spacecraft, there are two magnetic torquers. At the magnetometers, these torquers can generate magnetic fields larger than the ambient fields to be measured. Therefore signals from these torquer currents need to be removed. The torquer currents are measured at the same rate as the magnetometer rate, and the currents are used to correct the magnetometer measurements. However, the torquer currents were not low-pass filtered. As a result, large instantaneous steps in the torquer currents show up in the magnetometer data as a delayed, slowly rising wave with some ringing, just what one would expect from the magnetometer low-pass filters. The so-called ?Farthing coefficients? simulate, from a short past history of the torquer measurements, the effects of the magnetometer filters. The torquer current changes are asynchronous with the telemetry frames and the timing between these events must be measured to a eighth of a telemetry frame interval for good performance. The transient responses in changes in torquer currents are reduced, but not eliminated for large changes in torquer currents. There exists one opportunity at the beginning of each mission to perform a spacecraft rotation maneuver to determine magnetometer offsets. These offsets are used through the duration of each satellite's lifetime. Approximate coefficients are: * 0.8 milliampere per torquer current count * 4 counts per torquer current command step (3.2 milliampere per command step) * 410 milliamperes full scale current * 32 magnetometer counts per nT (approximate) * 8 torquer step counts can be up to approximately 0.5 nT (depends on axis, which torquer, which satellite, etc.)

16) GOES 11 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/A/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected alpha-particle fluxes for several energy ranges.

17) GOES 11 Space Evironment Monitor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/G/PT1M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:1 minute
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 1 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

18) GOES 11 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/G/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

19) GOES 11 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/H/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton and alpha particle fluxes for several energy ranges.

20) GOES 11 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/I/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

21) GOES 11 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/SEM/Z/PT5M
Start:2000-07-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2010-12-31 00:00:00 Instrument:Environment Monitor Resource:NumericalData
This GOES 11 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

22) GOES 12 Energetic Particle Sensor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/EPS/PT1M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:1 minute
Stop:2010-08-31 23:59:59 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
The energetic particle sensor data consists of electron and proton data. The electrons consists of 3 energy flux channels with energies greater than 0.6 MeV. The proton fluxes consist of 7 energy channels from 0.6 to 500 MeV.

23) GOES 12 Energetic Particle Sensor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/EPS/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-08-31 23:59:59 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
The energetic particle sensor data consists of electron, proton, and alpha particle data. The electrons consists of 3 energy flux channels with energies greater than 0.6 MeV. The protons consist of 7 energy channels from 0.6 to 500 MeV and the alpha particles consist of 6 energy channels from 4 to 500 MeV.

24) GOES 12 High Energy Proton and Alpha Detector (HEPAD) data at 5 m Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/HEPAD/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-08-31 23:59:59 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
The GOES 12 High Energy Proton and Alpha Detector (HEPAD) provides flux measurements of high energy proton and alpha particles. This data set consists of protons in 4 energy channels from 350 to >700 MeV and the alpha particles consist of 2 energy channels from 2560 to >3400 MeV.

25) GOES 12 high-resolution magnetometer data maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/MAG/PT0.512S
Start:2007-09-15 23:59:58 Observatory:GOES 12 Cadence:0.512 seconds
Stop:2008-06-30 23:59:58 Instrument:GOES 12, Triaxial Fluxgate Magnetometer Resource:NumericalData
GOES 12 magnetic field data at 0.512 second time resolution. The vector magnetic field is given in the spacecraft (s/c) earth-referenced coordinate system: Hp, He, Hn, and Ht, where Hp is perpendicular to the satellite orbital plane, or parallel to Earth's spin axis in the case of a zero degree inclination orbit; He is perpendicular to Hp and directed earthwards; Hn is perpendicular to both Hp and He and directed eastwards; and Ht is the total field. This data product also provides GOES 12 satellite positions and velocities derived from SSCWEB GEI ephemeris, interpolated to one minute time resolution. The magnetometer data are downlinked from the spacecraft in real-time to the NOAA Space Weather Prediction Center (SWPC) in Boulder, CO. The data from the raw Command and Data Acquisition (CDA) telemetry stream are processed by pre-processors at SWPC and from there 1-minute averages are distributed to SWPC Space Weather Operations, as well a archived at NOAA?s National Geophysical Data Center (NGDC) and NASA?s Coordinated Data Analysis Web (http://cdaweb.gsfc.nasa.gov/). The raw high-resolution data are corrected and processed at NOAA?s SWPC, and later archived at NGDC. The major issue for processing the high-resolution data is correction for the magnetic signature of spacecraft torquer currents as briefly discussed in the magnetometer instrument descriptions. In normal operation, the magnetometer samples its three axes every 0.512 seconds, synchronized with the telemetry frames. The magnetometer has an anti-aliasing low-pass filter on each axis. As part of the attitude control on the spacecraft, there are two magnetic torquers. At the magnetometers, these torquers can generate magnetic fields larger than the ambient fields to be measured. Therefore signals from these torquer currents need to be removed. The torquer currents are measured at the same rate as the magnetometer rate, and the currents are used to correct the magnetometer measurements. However, the torquer currents were not low-pass filtered. As a result, large instantaneous steps in the torquer currents show up in the magnetometer data as a delayed, slowly rising wave with some ringing, just what one would expect from the magnetometer low-pass filters. The so-called ?Farthing coefficients? simulate, from a short past history of the torquer measurements, the effects of the magnetometer filters. The torquer current changes are asynchronous with the telemetry frames and the timing between these events must be measured to a eighth of a telemetry frame interval for good performance. The transient responses in changes in torquer currents are reduced, but not eliminated for large changes in torquer currents. There exists one opportunity at the beginning of each mission to perform a spacecraft rotation maneuver to determine magnetometer offsets. These offsets are used through the duration of each satellite's lifetime. Approximate coefficients are: * 0.8 milliampere per torquer current count * 4 counts per torquer current command step (3.2 milliampere per command step) * 410 milliamperes full scale current * 32 magnetometer counts per nT (approximate) * 8 torquer step counts can be up to approximately 0.5 nT (depends on axis, which torquer, which satellite, etc.)

26) GOES 12 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/A/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected alpha-particle fluxes for several energy ranges.

27) GOES 12 Space Evironment Monitor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/G/PT1M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:1 minute
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 1 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

28) GOES 12 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/G/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton fluxes for several energy ranges.

29) GOES 12 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/H/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the uncorrected proton and alpha particle fluxes for several energy ranges.

30) GOES 12 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/I/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

31) GOES 12 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/SEM/Z/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-09-30 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 12 SEM data set contains various parameters at 5 min resolution. Within the data files is the Xray flux for two wavelength ranges, the magnetic field vectors, the >2 MeV uncorrected elecron fluxes, and the corrected proton fluxes for several energy ranges.

32) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/apead_cpflux_PT5M
Start:2011-09-01 00:00:00 Observatory:GOES 13 Cadence:5 minutes
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 15 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes from B detector. Data files contain long descriptive header.

33) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) alpha particle fluxes data at 32 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_a16e_PT32S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:32 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the alpha particle fluxes from B detector. Data files contain long descriptive header.

34) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) alpha particle fluxes data at 60 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_a16ew_PT1M
Start:2011-09-01 00:00:00 Observatory:GOES 13 Cadence:1 minute
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the alpha particle fluxes from B detector. Data files contain long descriptive header.

35) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) alpha particle fluxes data at 32 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_a16w_PT32S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:32 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. for more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the alpha particle fluxes from A detector. Data files contain long descriptive header.

36) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) electron fluxes data at 1 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_e13ew_PT1M
Start:2011-01-01 00:00:00 Observatory:GOES 13 Cadence:1 minute
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron fluxes with energy with >.8 MeV from both the A and B detectors. Data files contain long descriptive header.

37) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) electron fluxes data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_e13ew_PT5M
Start:2011-01-01 00:00:00 Observatory:GOES 13 Cadence:5 minutes
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron fluxes with energy with >.8 MeV from both the A and B detectors. Data files contain long descriptive header.

38) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) electron fluxes data at 4 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_e1ew_PT4S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:4 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron fluxes with energy with >.8 MeV from both the A and B detectors. Data files contain long descriptive header.

39) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) electron fluxes data at 16 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_e2ew_PT16S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:16 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron fluxes with energy with >2 MeV from both the A and B detectors. Data files contain long descriptive header.

40) GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) electron fluxes data at 16 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_e3ew_PT16S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:16 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron fluxes with energy with >4 MeV from both the A and B detectors. Data files contain long descriptive header.

41) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 1 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_p17ew_PT1M
Start:2011-01-01 00:00:00 Observatory:GOES 13 Cadence:1 minute
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes from B detector. Data files contain long descriptive header.

42) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_p17ew_PT5M
Start:2011-01-01 00:00:00 Observatory:GOES 13 Cadence:5 minutes
Stop:2013-04-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes from B detector. Data files contain long descriptive header.

43) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 8 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_p1ew_PT8S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:4 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes with energies from .74-4.2 MeV from both the A and B detectors. Data files contain long descriptive header.

44) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 32 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_p27e_PT32S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:32 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes from B detector. Data files contain long descriptive header.

45) GOES 13 Energetic Proton, Electron and Alpha Detector (EPEAD) proton fluxes data at 32 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/epead_p27w_PT32S
Start:2008-03-01 00:00:00 Observatory:GOES 13 Cadence:32 seconds
Stop:2013-04-09 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Energetic Proton, Electron and Alpha Detectors (EPEAD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. There are two EPEADs on each satellite, one looking east and one looking west. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton fluxes from A detector. Data files contain long descriptive header.

46) GOES 13 Magnetospheric Electron Detector (MAGED) data at 2 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/maged_19me1_PT2S
Start:2009-05-04 00:00:00 Observatory:GOES 13 Cadence:2 seconds
Stop:2013-06-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Magnetospheric Electron Detector (MAGED) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron count rates and fluxes from 30-50 keV. Data files contain long descriptive header.

47) GOES 13 Magnetospheric Electron Detector (MAGED) data at 2 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/maged_19me2_PT2S
Start:2009-05-04 00:00:00 Observatory:GOES 13 Cadence:2 seconds
Stop:2013-06-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Magnetospheric Electron Detector (MAGED) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron count rates and fluxes from 50-100 keV. Data files contain long descriptive header.

48) GOES 13 Magnetospheric Electron Detector (MAGED) data at 4 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/maged_19me3_PT4S
Start:2009-05-04 00:00:00 Observatory:GOES 13 Cadence:4 seconds
Stop:2013-06-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Magnetospheric Electron Detector (MAGED) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron count rates and fluxes from 100-200 keV. Data files contain long descriptive header.

49) GOES 13 Magnetospheric Electron Detector (MAGED) data at 32 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/maged_19me5_PT32S
Start:2009-05-04 00:00:00 Observatory:GOES 13 Cadence:32 seconds
Stop:2013-06-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Magnetospheric Electron Detector (MAGED) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the electron count rates and fluxes from 350-600 keV. Data files contain long descriptive header.

50) GOES 13 Magnetospheric Proton Detector (MAGPD) data at 16 s Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/13/EPEAD/magpd_19mp1_PT16S
Start:2009-05-04 00:00:00 Observatory:GOES 13 Cadence:16 seconds
Stop:2013-06-30 23:59:00 Instrument:Energetic Particle Monitor Resource:NumericalData
The GOES 13 Magnetospheric Proton Detector (MAGPD) are essentially the same as the Energetic Particle Sensor (EPS) on GOES 8-12. For more information, please see T. G. Onsager et al. (1996), Operational uses of the GOES energetic particle detectors, in GOES-8 and Beyond, Proc. SPIE, Vol. 2812, edited by E. R. Washwell, pp. 281-290, Bellingham, WA. These data file contain mainly information on the proton count rates and fluxes from 80-110 keV. Data files contain long descriptive header.

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