Exos B [ISAS]
This mission was part of the Japanese contribution to the International Magnetospheric Study, and it carried out coordinated observations with Exos A (Kyokko). Investigations of correlated mechanisms between particles and fields and plasma turbulence were made with in situ measurement techniques using electrostatic particle analyzers. The spacecraft, a 12-sided polyhedron, carried extendable dipole antennas with lengths of 103 m and 69.6 m, and a 1-m boom for a vector magnetometer. A solar panel array provided 30 W into a battery and regulator system. The spacecraft spin stabilized at 150 rpm but dropped to 3 rpm when the two sets of antennas were extended. Attitude was measured with a sun sensor to an accuracy of 0.5 deg. A 0.5 W136 MHz PCM/PM telemetry system handled 256 or 1024 bps, and a 2 W400 MHz PM system handled wideband 10 kHz or 3 kHz data. Data acquisition was in real time except for a 10-Kbyte memory for housekeeping and plasma parameter data.
The scientific instrumentation was:
Exos B operated until 1985 and reentered in April 2018.
Nation: | Japan |
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Type / Application: | Research, upper atmosphere, plasma |
Operator: | ISAS |
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Equipment: | |
Configuration: | |
Propulsion: | |
Power: | Solar cells, batteries |
Lifetime: | |
Mass: | 92 kg |
Orbit: | 230 km × 30558 km, 31° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Exos B (Jikiken) | 1978-087A | 16.09.1978 | Ka LP-M | M-3H [KM-?] |