The MUSES-A spacecraft mission objectives are to study the effect of a double lunar swingby technique, lunar orbital insertion, obtain experience using optical navigation equipment, measure mass and momentum of micrometeoroids by using a particle dust counter, and to support a packet telemetry and Reed-Solomon coding experiment by using a newly developed fault tolerant onboard computer. A flight profile is given, and information is presented in tabular form on the following topics: Deep Space Network support, frequency assignments, telemetry, command, and tracking support responsibility.
MUSES-A
1991
4 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Deep space network , Ground support systems , Japanese spacecraft , Spacecraft tracking , Japanese space program , Space missions , Airborne/spaceborne computers , Coding , Fault tolerance , Flight paths , Frequency assignment , Micrometeoroids , Momentum , Navigation aids , Optical equipment , Orbit insertion , Radiation counters , Swingby technique , Telemetry , Foreign technology
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