Spacecraft system and subsystem designs at the conceptual level to perform either of two Mars Orbiter missions, a Climatology Mission and an Aeronomy Mission were developed. The objectives of these missions are to obtain and return data.
Mars orbiter conceptual systems design study
1982-09-20
Report
No indication
English
Mars Orbiter Conceptual Systems Design Study
NTIS | 1982
|Springer Verlag | 2013
|NTRS | 1998
Mars Orbiter Sample Return Power Design
NTRS | 2005
|