This page summarizes information about the selected resource and its origin based on SPASE metadata.
SPASE version 2.0.0
This data set contains the investigator-selected Key Parameters from the Magnetic Field instrument (MGF) on Geotail, as made available via NSSDC's interactive WWW interface CDAWeb.
Selected references:
Kokubun, S., et al., Magnetic field measurement (MGF), In Geotail Prelaunch Report, SES-TD-92-007SY, Institute of Space and Astronautical Science, SES Data Center, pp. 58-70, Apr. 1992.
Nishida, A., et al., Geotail mission to explore earth's magnetotail, EOS, 73, No. 40, Oct. 1992.
Kokubun, S., et al., The GEOTAIL Magnetic Field Experiment, J. Geomag. Geoelectr., 46, No. 1, 7-21, 1994.
Reprint of Kokubun, S., T. Yamamoto, M. H. Acuna, K. Hayashi, K. Shiokawa, and H. Kawano, The Geotail Magnetic Field Experiment, J. Geomag. Geoelectr., 46, 7-21, 1994.
Data were provided by T. Nagai at Institute of Space and Astronautical Science, JAXA in Japan.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Prof. Tsugunobu Nagai |
| 2. | Scientist | Dr. Donald H. Fairfield |
| 3. | Metadata contact | Jan Merka |
Switched from outer magnetometer to inner in January 2007.
This data is computed with a preliminary algorithm and is not necessarily complete nor is it certified by the experimenters or considered publishable.
Time in miliseconds since CDF epoch
Time as an array (year, day of year and elapsed milliseconds of day).
| Index | Name | Units | Valid min | Valid max | Fill value |
|---|---|---|---|---|---|
| 1 | Year | year | 1992 | 2020 | -2147483648 |
| 2 | Day of Year (jan 1 = day 1) | day | 1 | 366 | -2147483648 |
| 3 | Elapsed ms of day | ms | 0 | 86399000 | -2147483648 |
Elapsed milliseconds of day
Observed magnetic field intensity
Observed magnetic field vector in GSE coordinates
| Index | Name | Component | Valid min | Valid max | Fill value |
|---|---|---|---|---|---|
| 1 | Bx | I | -32768 | 32767 | -32768 |
| 2 | By | J | -32768 | 32767 | -32768 |
| 3 | Bz | K | -32768 | 32767 | -32768 |
Standard deviation of sin fitting for magnetic field in sensor coordinates
| Index | Name | Component | Valid min | Valid max | Fill value |
|---|---|---|---|---|---|
| 1 | Bx-RMS | I | -32768 | 32767 | -32768 |
| 2 | By-RMS | J | -32768 | 32767 | -32768 |
| 3 | Bz-RMS | K | -32768 | 32767 | -32768 |
Range status of the fluxgate magnetometer.
Satellite position vector in GSE coordinates
| Index | Name | Component | Valid min | Valid max | Fill value |
|---|---|---|---|---|---|
| 1 | X-GSE | I | -1800000.0 | 1800000.0 | -1.0E31 |
| 2 | Y-GSE | J | -1800000.0 | 1800000.0 | -1.0E31 |
| 3 | Z-GSE | K | -1800000.0 | 1800000.0 | -1.0E31 |
Data quality flag: Good/Bad/Fill (0: good; 1,2,3: poor 4: fill value)
Post gap flag. 0: no gap occurred; 1: gap occurred because SIRIUS data were illegal or because the instrument was not in a mode that allowed KP's 2: gap occurred because of the jump of MGF RANGE or MGF SENSE during 64 s
SPASE version 2.0.0
The objective of this experiment is to measure the magnetic field variation of the magnetotail in the frequency below 50 Hz. The MGF experiment consists of dual three-axis fluxgate magnetometers and a three-axis search coil magnetometer. Triad fluxgate sensors, which utilize a ring core geometry, are installed at the end and middle of a 6 m deployable mast. Three search coils are mounted approximately one-half of the way out on another 6 m boom together with search coils for the VLF wave in the PWI system.
The fluxgate magnetometers are of standard design and consist of an amplifier, filter, phase sensitive detector, integrator, and a voltage-current convertor. The fluxgate magnetometers operate in seven dynamic ranges to cover various regions of the Earth's magnetosphere and the solar wind: +/-16 nT, +/-64 nT, +/-256 nT, +/-1024 nT, +/-4096 nT, +/-16384 nT, and +/-65536 nT, and supply 16 vectors/sec.
The automatic range control of the fluxgate magnetometers failed in 1999 so the observable range was manually fixed in the +/-256 nT where it has remained ever since. On November 23, 2006, the fluxgate magnetometer at the end of the boom failed and data from the second magnetometer at the middle of the boom has been used ever since. Neither of the above changes substantially affect the data.
The search coil magnetometer system consists of three sensors, preamplifier, amplifier, filter, multiplexer, and an A/D converter. The search coil magnetometers operate in a frequency range of 0.5 kHz to 1 kHz, and supply 128 vectors/sec. The fluxgate magnetometer operates in both real time and record modes, while the search coil data are used only in real time mode.
Information about the Magnetic Fields Measurement (MGF)
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Prof. Tsugunobu Nagai |
| 2. | Scientist | Dr. Donald H. Fairfield |
| 3. | Metadata contact | Jan Merka |
SPASE version 2.0.0
The solar wind draws the Earth's magnetic field into a long tail on the nightside of the Earth and stores energy in the stretched field lines of the magnetotail. During active periods, the tail couples with the near-Earth magnetosphere, sometimes releasing energy stored in the tail and activating auroras in the polar ionosphere.
The Geotail mission measures global energy flow and transformation in the magnetotail to increase understanding of fundamental magnetospheric processes. This includes the physics of the magnetopause magnetospheric boundary regions, the lobe and plasma sheet, and reconnection and neutral line formation, i.e., the mechanisms processes of input, transport, storage, release and conversion of mass, momentum and energy in the magnetotail.
Geotail, together with Wind, Polar, SOHO, and Cluster projects, constitute a cooperative scientific satellite project designated the International Solar Terrestrial Physics (ISTP) program which aims at gaining improved understanding of the physics of solar-terrestrial relations.
Geotail is a spin-stabilized spacecraft utilizing mechanically despun antennas with a design lifetime of about four years. The nominal spin rate of the spacecraft is about 20 rpm around a spin axis maintained between 85-89 degrees to the ecliptic plane. Geotail is cylindrical, approximately 2.2 m in diameter, and 1.6 m high. with It has body-mounted solar cells. Geotail also has and a back-up battery subsystem which that operates when the spacecraft is in the Earth's shadow (limited to 2 hrs). Real-time telemetry data transmitted in X-band are received at the Usuda Deep Space Center (UDSC) in Japan. There are two tape recorders on board, each with a capacity of 450 Mb, which allows daily 24-hour data coverage and are collected in playback mode by the NASA Deep Space Network (DSN).
The Geotail mission is divided into two phases. During the two-year initial phase, the orbit apogee was kept on the nightside of the Earth by using the Moon's gravity in a series of double-lunar swing-by maneuvers that result in the spacecraft spending most of its time in the distant magnetotail (maximum apogee about 200 Earth radii) with a period varying from one to four months. Then, in November 1994, there were a series of maneuvers that reduced the apogee to 50 Re. After three more months in the magnetotail the spacecraft was put in a 10 by 30 Re orbit where it has remained except that the perigee was reduced from 10 to 9 Re in June 1997.
Details on the Geotail mission and instrumentation are given in the Journal of Geomagnetism and Geoelectricity (Vol. 46, No. 1, 1994); online from JGG at
http://www.terrapub.co.jp/journals/EPS/JGG
Information about the Geotail mission
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Guan Le |
| 2. | Project scientist | Prof. Masaki Fujimoto |
| 3. | Metadata contact | Jan Merka |
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 2.0.0
SPASE version 1.2.0
Coordinated Data Analysis Web (CDAWeb) supports not only interactive plotting of variables from multiple instruments on multiple investigations simultaneously on arbitrary, user-defined time-scales. It also supports data retrieval in various formats using its interactive web interface or ftp service.
Coordinated Data Analysis Web (CDAWeb) home page at Space Physics Data Facility of the NASA Goddard Space Flight Center.
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. Robert E. McGuire |