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1) AMPTE/CCE Spin-averaged Magnetic Field Measurements maxmize
Resource ID:spase://VMO/NumericalData/AMPTE_CCE/MFE/PT5.83S
Start:1984-08-20 23:59:54 Observatory:AMPTE/CCE Cadence:5.83 seconds
Stop:1989-01-09 23:59:34 Instrument:AMPTE/CCE Magnetic Field Experiment (MFE) Resource:NumericalData
AMPTE/CCE spin-averaged DC magnetic field at ~5.83 second resolution.

2) AMPTE/IRM Magnetic Field maxmize
Resource ID:spase://VMO/NumericalData/AMPTE_IRM/MAG/PT4.4S
Start:1984-08-21 00:48:41 Observatory:AMPTE/IRM Cadence:4.4 seconds
Stop:1986-08-11 21:45:07 Instrument:AMPTE/IRM Magnetometer Resource:NumericalData
AMPTE/IRM spin-averaged magnetic field at ~4.4 second resolution.

3) AMPTE/UKS Magnetic Field Data maxmize
Resource ID:spase://VMO/NumericalData/AMPTE_UKS/FGM/PT5S
Start:1984-08-21 08:24:42 Observatory:AMPTE/UKS Cadence:5 seconds
Stop:1985-01-15 08:01:02 Instrument:AMPTE/UKS Magnetometer Resource:NumericalData
AMPTE/UKS 5-second (spin) averaged magnetic field measurements

4) IMP 8 bow shock crossings maxmize
Resource ID:spase://VMO/Catalog/BS_IMP8
Start:1973-10-31 07:31:00 Observatory:IMP 8 Cadence:
Stop: Instrument:IMP 8 Magnetic Field Experiment Resource:Catalog
A complete list of bow shock crossings observed by IMP 8 spacecraft. The shock crossings were manually identified in magnetic field and/or thermal plasma measurements by J. Merka, A. Szabo, K. Paularena, J. Richardson, and T. Narock. Each identified crossing was reviewed by at least two persons from the team. Upstream parameters are as measured by IMP 8 on the solar wind side of the shock, typically over a few-minute interval judged by the IMP field and plasma teams as stable. For multiple-shock records, all upstream parameters are for the first shock crossing. Downstream parameters are as measured by IMP 8 on the magnetosheath side of the shock, typically over a few-minute interval. For a multiple-shock records, all downstream parameters are for the first shock crossing if possible.

5) CRRES 2s magnetic field data maxmize
Resource ID:spase://VMO/NumericalData/CRRES/MAG/PT2S
Start:1990-10-11 00:00:00 Observatory:CRRES Cadence:2 seconds
Stop:1991-10-13 00:00:00 Instrument:Fluxgate Magnetometer Resource:NumericalData
This data set contains magnetic field vectors and tilt angles from the CRRES tri-axial fluxgate magnetometer data. The magnetic field vectors are at 2 s resolution and in the Vehicle Dipole Horizon (VDH) coordinate system. Also included are the magnetic field magnitude and the tilt of the magnetic field in Theta and Phi in the VDH coordinate system.

6) CRRES 30s magnetic field data maxmize
Resource ID:spase://VMO/NumericalData/CRRES/MAG/PT30S
Start:1990-10-11 00:00:00 Observatory:CRRES Cadence:30 seconds
Stop:1991-10-13 00:00:00 Instrument:Fluxgate Magnetometer Resource:NumericalData
This data set contains spin fitted magnetic field vectors and magnitudes from the CRRES tri-axial fluxgate magnetometer data. The magnetic field vectors are at 30 s resolution and in the GSE coordinate system.

7) Cluster Rumba Spin Resolution Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Rumba/FGM/SpinResolution/4S
Start:2001-01-30 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:4 seconds
Stop:2014-04-20 01:02:10 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster Rumba spacecraft.

8) Cluster II Rumba Unvalidated Prime Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Rumba/FGM/UnvalidatedParameter/4S
Start:2006-01-01 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:4 seconds
Stop:2014-04-20 01:02:10 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution unvalidated prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 Rumba spacecraft. Unvalidated FGM data might sometimes contain artefacts such as spikes (duration ~ 1 spin), or short rotations (few spins). Very occasionally the data contain many spikes over several hours. Please contact Elizabeth Lucek (e.lucek@imperial.ac.uk) for more information regarding possible artefacts in specific intervals of data. The unvalidated prime parameter Data Set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

9) Cluster II Rumba Prime Parameter Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Rumba/STAFF/PrimeParameter/4S
Start:2000-12-09 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:4 seconds
Stop:2014-04-20 01:02:10 Instrument:Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Resource:NumericalData
The Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) experiment provides magnetic field power spectral density values parallel and perpendicular to the magnetic field and the electric field power spectral density values for several frequency ranges. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The STAFF (Spatio-Temporal Analysis of Field Fluctuations) Experiment for the Cluster Mission, by N. Cornilleau-Wehrlin et al., from which this information was obtained.

10) Cluster Salsa Spin Resolution Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Salsa/FGM/SpinResolution/4S
Start:2001-01-30 00:00:00 Observatory:Cluster FM6 (Salsa) Cadence:4 seconds
Stop:2014-04-20 01:01:14 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster Salsa spacecraft.

11) Cluster II Salsa Unvalidated Prime Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Salsa/FGM/UnvalidatedParameter/4S
Start:2006-01-01 00:00:00 Observatory:Cluster FM6 (Salsa) Cadence:4 seconds
Stop:2014-04-20 01:01:14 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution unvalidated prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 Salsa spacecraft. Unvalidated FGM data might sometimes contain artefacts such as spikes (duration ~ 1 spin), or short rotations (few spins). Very occasionally the data contain many spikes over several hours. Please contact Elizabeth Lucek (e.lucek@imperial.ac.uk) for more information regarding possible artefacts in specific intervals of data. The unvalidated prime parameter Data Set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

12) Cluster II Salsa Prime Parameter Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Salsa/STAFF/PrimeParameter/4S
Start:2000-12-09 00:00:00 Observatory:Cluster FM6 (Salsa) Cadence:4 seconds
Stop:2014-04-20 01:01:14 Instrument:Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Resource:NumericalData
The Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) experiment provides magnetic field power spectral density values parallel and perpendicular to the magnetic field and the electric field power spectral density values for several frequency ranges. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The STAFF (Spatio-Temporal Analysis of Field Fluctuations) Experiment for the Cluster Mission, by N. Cornilleau-Wehrlin et al., from which this information was obtained.

13) Cluster Samba Spin Resolution Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Samba/FGM/SpinResolution/4S
Start:2001-01-30 00:00:00 Observatory:Cluster FM7 (Samba) Cadence:4 seconds
Stop:2014-04-20 01:01:50 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster Samba spacecraft.

14) Cluster II Samba Unvalidated Prime Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Samba/FGM/UnvalidatedParameter/4S
Start:2006-01-01 00:00:00 Observatory:Cluster FM7 (Samba) Cadence:4 seconds
Stop:2014-04-20 01:01:49 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution unvalidated prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 Samba spacecraft. Unvalidated FGM data might sometimes contain artefacts such as spikes (duration ~ 1 spin), or short rotations (few spins). Very occasionally the data contain many spikes over several hours. Please contact Elizabeth Lucek (e.lucek@imperial.ac.uk) for more information regarding possible artefacts in specific intervals of data. The unvalidated prime parameter Data Set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

15) Cluster II Samba Prime Parameter Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Samba/STAFF/PrimeParameter/4S
Start:2000-12-09 00:00:00 Observatory:Cluster FM7 (Samba) Cadence:4 seconds
Stop:2014-04-20 01:01:50 Instrument:Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Resource:NumericalData
The Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) experiment provides magnetic field power spectral density values parallel and perpendicular to the magnetic field and the electric field power spectral density values for several frequency ranges. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The STAFF (Spatio-Temporal Analysis of Field Fluctuations) Experiment for the Cluster Mission, by N. Cornilleau-Wehrlin et al., from which this information was obtained.

16) Cluster Tango Spin Resolution Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Tango/FGM/SpinResolution/4S
Start:2001-01-30 00:00:00 Observatory:Cluster FM8 (Tango) Cadence:4 seconds
Stop:2014-04-20 01:01:39 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster Tango spacecraft.

17) Cluster II Tango Unvalidated Prime Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Tango/FGM/UnvalidatedParameter/4S
Start:2006-01-01 00:00:00 Observatory:Cluster FM8 (Tango) Cadence:4 seconds
Stop:2014-04-20 01:01:39 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains spin resolution unvalidated prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 Tango spacecraft. Unvalidated FGM data might sometimes contain artefacts such as spikes (duration ~ 1 spin), or short rotations (few spins). Very occasionally the data contain many spikes over several hours. Please contact Elizabeth Lucek (e.lucek@imperial.ac.uk) for more information regarding possible artefacts in specific intervals of data. The unvalidated prime parameter Data Set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

18) Cluster II Tango Prime Parameter Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster-Tango/STAFF/PrimeParameter/4S
Start:2000-12-09 00:00:00 Observatory:Cluster FM8 (Tango) Cadence:4 seconds
Stop:2014-04-20 01:01:39 Instrument:Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Resource:NumericalData
The Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) experiment provides magnetic field power spectral density values parallel and perpendicular to the magnetic field and the electric field power spectral density values for several frequency ranges. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The STAFF (Spatio-Temporal Analysis of Field Fluctuations) Experiment for the Cluster Mission, by N. Cornilleau-Wehrlin et al., from which this information was obtained.

19) Cluster II Summary Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster/FGM/SummaryParameter/60S
Start:2001-01-01 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:60 seconds
Stop:2014-04-20 01:01:13 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains 1 minute resolution validated summary prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 spacecraft. The summary prime parameter data set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

20) Cluster II Unvalidated Summary Parameter Fluxgate Magnetometer (FGM) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster/FGM/UnvalidatedSummaryParameter/60S
Start:2006-01-01 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:60 seconds
Stop:2014-04-20 01:01:13 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
This dataset contains 1 minute resolution unvalidated summary prime parameter measurements of the magnetic field vector from the fluxgate magnetometer (FGM) instrument on the Cluster 2 spacecraft. Unvalidated FGM data might sometimes contain artefacts such as spikes (duration ~ 1 spin), or short rotations (few spins). Very occasionally the data contain many spikes over several hours. Please contact Elizabeth Lucek (e.lucek@imperial.ac.uk) for more information regarding possible artefacts in specific intervals of data. The unvalidated summary prime parameter data set does not contain the spacecraft position data or additional range and telemetry mode information that the CAA parameter data set does contain.

21) Cluster II Summary Parameter Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Data maxmize
Resource ID:spase://VMO/NumericalData/Cluster/STAFF/SummaryParameter/60S
Start:2001-01-09 00:00:00 Observatory:Cluster FM5 (Rumba) Cadence:60 seconds
Stop:2014-04-20 01:01:14 Instrument:Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) Resource:NumericalData
The Spatio-Temporal Analysis of Magnetic Field Fluctuations (STAFF) experiment provides magnetic field power spectral density values parallel and perpendicular to the magnetic field and the electric field power spectral density values for several frequency ranges. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The STAFF (Spatio-Temporal Analysis of Field Fluctuations) Experiment for the Cluster Mission, by N. Cornilleau-Wehrlin et al., from which this information was obtained.

22) Dynamics Explorer 1 Magnetic Field Observations Triaxial Fluxgate Magnetometer (MAG-A) maxmize
Resource ID:spase://VMO/NumericalData/DE1/MAGA/PT0.062S
Start:1981-09-15 00:00:00 Observatory:Dynamics Explorer 1 Cadence:0.062 seconds
Stop:1991-02-18 00:00:00 Instrument:Magnetic Field Observations (MAG-A) Resource:NumericalData
Dynamics Explorer 1 Magnetic Field Observations Triaxial Fluxgate Magnetometer

23) DE 1 Magnetic Field Observations Triaxial Fluxgate Magnetometer (MAG-A) maxmize
Resource ID:spase://VMO/NumericalData/DE1/MAGA/PT6S
Start:1981-09-15 00:00:00 Observatory:Dynamics Explorer 1 Cadence:6 seconds
Stop:1991-02-18 00:00:00 Instrument:Magnetic Field Observations (MAG-A) Resource:NumericalData
Dynamics Explorer 1 Magnetic Field Observations Triaxial Fluxgate Magnetometer at 6 second resolution.

24) Dynamics Explorer 2 Magnetic Field Observations Triaxial Fluxgate Magnetometer (MAG-B) maxmize
Resource ID:spase://VMO/NumericalData/DE2/MAGB/PT0.062S
Start:1981-09-15 00:00:00 Observatory:Dynamics Explorer 2 Cadence:0.062 seconds
Stop:1981-02-19 00:00:00 Instrument:Magnetic Field Observations (MAG-B) Resource:NumericalData
Dynamics Explorer 2 Magnetic Field Observations Triaxial Fluxgate Magnetometer

25) Double Star 1 Spacecraft Flux Gate Magnetometer (FGM) Prime Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar1/FGM/PrimeParameters/4S
Start:2004-01-08 03:43:36 Observatory:Double Star 1 Cadence:4 seconds
Stop:2007-09-16 10:41:55 Instrument:FGM (Flux Gate Magnetometer) Resource:NumericalData
The Double Star 1 Flux Gate Magnetometer (FGM) prime parameter data set contains various parameters in GSE coordinates at spin resolution. These parameters include universal time, the instrument status, the magnetic field vector in GSE coordinates, and the magnetic field variances. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

26) Double Star 1 Spacecraft Flux Gate Magnetometer (FGM) Summary Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar1/FGM/SummaryParameters/60S
Start:2004-01-08 03:44:30 Observatory:Double Star 1 Cadence:60 seconds
Stop:2007-09-19 22:40:30 Instrument:FGM (Flux Gate Magnetometer) Resource:NumericalData
The Double Star 1 Flux Gate Magnetometer (FGM) summary parameter data set contains various parameters in GSE coordinates at 60 s resolution. These parameters include universal time, the instrument status, the magnetic field vector in GSE coordinates, and the magnetic field variances. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

27) Double Star 1 Spacecraft Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor (STAFF-DWP) Prime Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar1/STAFF-DWP/PrimeParameters/4S
Start:2004-01-08 03:43:36 Observatory:Double Star 1 Cadence:4 seconds
Stop:2007-09-16 10:41:55 Instrument:STAFF-DWP (Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor Resource:NumericalData
The Double Star 1 Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor prime parameter data set contains various parameters at spin resolution. These parameters include universal time, the instrument status, and magnetic field spectral power from FGM data for various frequency ranges. Frequency ranges not clear. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

28) Double Star 1 Spacecraft Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor (STAFF-DWP) Summary Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar1/STAFF-DWP/SummaryParameters/60S
Start:2004-01-08 03:43:36 Observatory:Double Star 1 Cadence:60 seconds
Stop:2007-09-16 10:41:55 Instrument:STAFF-DWP (Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor Resource:NumericalData
The Double Star 1 Spatio-Temporal Analyzer of Field Fluctuations and Digital Wave Processor summary parameter data set contains various parameters at 60 s. These parameters include universal time, the instrument status, and magnetic field spectral power from FGM data for various frequency ranges. Frequency ranges not clear. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

29) Double Star 2 Spacecraft Flux Gate Magnetometer (FGM) Prime Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar2/FGM/PrimeParameters/4S
Start:2004-07-30 07:00:49 Observatory:Double Star 2 Cadence:4 seconds
Stop:2008-05-31 18:59:05 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
The Double Star 2 Flux Gate Magnetometer (FGM) prime parameter data set contains various parameters in GSE coordinates at spin resolution. These parameters include universal time, the instrument status, the magnetic field vector in GSE coordinates, and the magnetic field variances. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

30) Double Star 2 Spacecraft Flux Gate Magnetometer (FGM) Summary Parameters Data maxmize
Resource ID:spase://VMO/NumericalData/DoubleStar2/FGM/SummaryParameters/60S
Start:2004-07-30 08:18:30 Observatory:Double Star 2 Cadence:60 seconds
Stop:2008-05-31 18:59:30 Instrument:Fluxgate Magnetometer (FGM) Resource:NumericalData
The Double Star 2 Flux Gate Magnetometer (FGM) summary parameter data set contains various parameters in GSE coordinates at 60 s resolution. These parameters include universal time, the instrument status, the magnetic field vector in GSE coordinates, and the magnetic field variances. These parameters are available through Double Star Science Data Centre The Data Ring with restricted access.

31) 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.

32) 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.)

33) 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.

34) GOES 10 Magnetic Field Sensor data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/MAG/PT5M
Start:1998-07-31 00:00:00 Observatory:GOES 10 Cadence:5 minutes
Stop:2009-12-31 23:59:00 Instrument:GOES 10, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. After temperature correction, and before (undescribed) stray-field correction, the accuracy is at about 1 nT level. Data files contain long descriptive header.

35) GOES 10 Magnetic Field Sensor data at 1 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/10/MAG/PT60S
Start:1998-07-31 00:00:00 Observatory:GOES 10 Cadence:1 minute
Stop:2009-12-31 23:59:00 Instrument:GOES 10, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. After temperature correction, and before (undescribed) stray-field correction, the accuracy is at about 1 nT level. Data files contain long descriptive header.

36) 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.)

37) GOES 11 Magnetic Field Sensor data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/MAG/PT5M
Start:2003-06-01 00:00:00 Observatory:GOES 11 Cadence:5 minutes
Stop:2011-02-28 23:59:00 Instrument:GOES 11, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. Data files contain long descriptive header.

38) GOES 11 Magnetic Field Sensor data at 1 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/11/MAG/PT60S
Start:2003-06-01 00:00:00 Observatory:GOES 11 Cadence:1 minute
Stop:2011-02-28 23:59:00 Instrument:GOES 11, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. Data files contain long descriptive header.

39) 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.)

40) GOES 12 Magnetic Field Sensor data at 5 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/MAG/PT5M
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:5 minutes
Stop:2010-08-31 23:59:00 Instrument:GOES 12, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. Data files contain long descriptive header.

41) GOES 12 Magnetic Field Sensor data at 1 min Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/12/MAG/PT60S
Start:2003-01-01 00:00:00 Observatory:GOES 12 Cadence:1 minute
Stop:2010-08-31 23:59:00 Instrument:GOES 12, Triaxial Fluxgate Magnetometer Resource:NumericalData
The magnetic field sensor, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 1000 nT (without saturation) and a resolution of 0.1 nT. Data files contain long descriptive header.

42) GOES 2 Magnetic Field Monitor at 3 sec Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/2/MFM/PT3S
Start:1977-08-01 00:00:00 Observatory:GOES 2 Cadence:3 seconds
Stop:1983-05-31 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.

43) GOES 3 Magnetic Field Monitor at 3 sec Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/3/MFM/PT3S
Start:1979-01-01 00:00:00 Observatory:GOES 3 Cadence:3 seconds
Stop:1980-08-31 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.

44) GOES 5 Biaxial Fluxgate Magnetometer at 3 sec Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/MAG/PT3S
Start:1983-01-01 00:00:00 Observatory:GOES 5 Cadence:3 seconds
Stop:1987-05-31 00:00:00 Instrument:Biaxial Fluxgate Magnetometer Resource:NumericalData
The spinning twin-fluxgate magnetometer, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 400 nT (without saturation) and a resolution of 0.1 nT over a range of +/- 50 nT. The sensitivity of the magnetometer was about 0.2 nT. The instrument and its electronics were carried on board GOES-4,-5,-6,and -7, without significant changes. Data during the first 3 months of 1986 has poor quality Hp component. The experiment became inoperational in February, 1987.

45) GOES 5 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/SEM/A/PT5M
Start:1986-01-01 00:00:00 Observatory:GOES 5 Cadence:5 minutes
Stop:1987-03-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 5 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.

46) GOES 5 Space Evironment Monitor Data at 1 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/SEM/G/PT1M
Start:1986-01-01 00:00:00 Observatory:GOES 5 Cadence:1 minute
Stop:1987-03-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 5 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.

47) GOES 5 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/SEM/G/PT5M
Start:1986-01-01 00:00:00 Observatory:GOES 5 Cadence:5 minutes
Stop:1987-03-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 5 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.

48) GOES 5 Space Evironment Monitor data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/SEM/I/PT5M
Start:1986-01-01 00:00:00 Observatory:GOES 5 Cadence:5 minutes
Stop:1987-03-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 5 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.

49) GOES 5 Space Evironment Monitor Data at 5 min Resolution maxmize
Resource ID:spase://VMO/NumericalData/GOES/5/SEM/Z/PT5M
Start:1986-01-01 00:00:00 Observatory:GOES 5 Cadence:5 minutes
Stop:1987-03-31 00:00:00 Instrument:Space Environment Monitor (SEM) Resource:NumericalData
This GOES 5 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.

50) GOES 6 Biaxial Fluxgate Magnetometer at 3 sec Resolution in Spacecraft Coordinates maxmize
Resource ID:spase://VMO/NumericalData/GOES/6/MAG/PT3S
Start:1983-05-01 00:00:00 Observatory:GOES 6 Cadence:3 seconds
Stop:1994-11-30 00:00:00 Instrument:Biaxial Fluxgate Magnetometer Resource:NumericalData
The spinning twin-fluxgate magnetometer, located at a few meters away from the spacecraft was designed to provide the orthogonal components of the magnetic field: Hp was parallel to the spin axis that was held nearly in the direction of Earth's axis, He was directed toward Earth center, and Hn pointed eastward. The magnetometer had a range of +/- 400 nT (without saturation) and a resolution of 0.1 nT over a range of +/- 50 nT. The sensitivity of the magnetometer was about 0.2 nT. The instrument and its electronics were carried on board GOES-4,-5,-6,and -7, without significant changes. Data during the first 3 months of 1986 has poor quality Hp component. The experiment became inoperational in February, 1987.

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