Moon revolving observation satellites

Details Moon revolving observation satellites Moon revolving observation satellites

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992fsa..workr....n&link_type=abstract

In its Future Space Activity Workshop: Lunar Base Workshop 1992 21 p (SEE N93-28014 10-12)

Computer Science

Japanese Spacecraft, Lunar Exploration, Lunar Landing, Lunar Landing Modules, Lunar Satellites, Mineral Exploration, Satellite Design, Spacecraft Equipment, Spacecraft Instruments, Data Acquisition, Data Processing, Extraterrestrial Resources, Lunar Maps, Radiometers, Remote Sensors, Satellite Control, Spacecraft Configurations, Spacecraft Power Supplies, Telecommunication

Scientific paper

The major mission objectives for the moon revolving observation satellites are lunar surface mapping and resources exploration, and soft landing experiment to the lunar surface. Missions to accomplish the objectives were studied on two mission cases, 2-ton moon revolving satellite and 1.5-ton moon revolving satellite plus 500 kg landing experiment module. Three kinds of mission models set up for each of the two mission cases are shown. The result of the mission analysis, including analyses on data acquisition and sensor operation plan, and system study, including studies of satellite configuration, and subsystem study, including the studies of attitude and orbit control, and solar paddle subsystems, are outlined.

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