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.


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    MUSES-A

    Nishimura, T. / Hayashi, T. | NTRS | 1991


    Muses-C project

    Fujiwara, A. / Tuschiya, K. | British Library Online Contents | 1996


    The Muses CN Rover

    Jones, R. / Wilcox, B. H. / Newell, M. A. et al. | NTRS | 1998


    REENTRY DYNAMICS OF MUSES-C

    Ishii, Nobuaki | Online Contents | 1998


    Planetary protection policy for MUSES-C

    Fujiwara, A. / Kawaguchi, J. / Uesugi, K. et al. | British Library Conference Proceedings | 2004