JIKIKEN (EXOS-B)

JIKIKEN (EXOS-B) - JAXA Spacecraft

The 12-sided polyhedron spacecraft JIKIKEN (EXOS-B) featured a 1-meter boom for a vector magnetometer in addition to extensible dipole antennae with lengths of 69.6 and 103 meters. 30 W were supplied to a battery and regulator system by a solar panel array.

With both sets of antennas extended, the spacecraft's spin decreased from 150 revolutions per minute to 3 revolutions per minute. A solar sensor was used to measure the angle with an accuracy of 0.5 degrees. Wideband 10 kHz or 3 kHz data was handled by a 2 W400 MHz PM system, while 256 or 1024 bps was handled by a 0.5 W136 MHz PCM/PM telemetry system. With the exception of a 10-Kbyte buffer used for housekeeping and plasma parameter data, data collecting was done in real time.

JIKIKEN (EXOS-B) Mission Information

Mission Details

NameJIKIKEN (EXOS-B)
TypeSpacecraft
ApplicationEarths magnetosphere observation satellite research on the region from the plasmasphere to the deep magnetosphere and participated in the International Magnetospheric Study (IMS) conducted from 1976 to 1979.
Launch DateSeptember 16, 1978
Launch SiteKagoshima Space Center (Uchinoura), Japan
Launch VehicleM-3H-3

Satellite Details

Scientific InstrumentParticle energy monitor, Electron beam radiation experiment instrument, Data processing unit (DPU)
Mass90 Kg
Shape60cm high, 75cm long from face to face, 50m- and 30m-long antennas with sensors

Orbit Information

OrbitHighly Elliptical Orbit
Orbital AltitudePerigee 220 Km, Apogee 30100 Km
Orbital Inclination31 Degrees
Orbital Period524 Minutes

Space Organization Details

OrganizationJAXA
ContinentAsia
CountryJapan

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