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
1991-10-01
Sonstige
Keine Angabe
Englisch
NTIS | 1991
|British Library Online Contents | 1996
|NTRS | 1998
|Online Contents | 1998
|Planetary protection policy for MUSES-C
British Library Conference Proceedings | 2004
|