A summary of the satellite operation conditions in the launch and early orbit operation phase and the results of the launch and early orbit phase operation and functional verification on the following subsystems of the JERS-1 (Japanese Earth Resources Satellite-1) is presented: (1) C & DH (Communication and Data Handling Subsystem); (2) EPS (Electrical Power Subsystem); (3) AOCS (Attitude and Orbit Control Subsystem); (4) RCS (Reaction Control Subsystem); (5) TCS (Thermal Control Subsystem); (6) SAR (Synthetic Aperture Radar); (7) OPS (Optical Sensor); (8) MDT (Mission Data Transmitter); and (9) MDR (Mission Data Recorder).
Chikyuu Shigen Eisei 1 Gou (JERS-1) Tsuiseki Kansei Gijutsu Shien Oyobi Hyouka Kaiseki (Flight Data Analysis of Japanese Earth Resources Satellite-1 (JERS-1))
1993
19 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Space Launch Vehicles & Support Equipment , Japanese spacecraft , Postlaunch reports , Spacecraft performance , Satellite control , Spacecraft equipment , Spacecraft instruments , Spacecraft launching , Propulsion system performance , Satellite ground support , Satellite guidance , Spacecraft power supplies , Spacecraft stability , Foreign technology
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