Conceptual design of the Mars Rover Sample Return system

Details Conceptual design of the Mars Rover Sample Return system Conceptual design of the Mars Rover Sample Return system

Jan 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989aiaa.meetq....r&link_type=abstract

AIAA, Aerospace Sciences Meeting, 27th, Reno, NV, Jan. 9-12, 1989. 9 p.

Physics

Interplanetary Flight, Mars Sample Return Missions, Mars Surface Samples, Mission Planning, Roving Vehicles, Aerocapture, Data Links, Information Systems, Space Navigation

Scientific paper

The results of the prephase A study of the Mars Rover Sample Return system are presented. Four mission scenarios are studied, two in the B-configuration, and two D-configuration missions. They incorporated variations in delivery-to-Mars mode, earth-return mode (propulsive or aerocapture), landing site latitude, and rover size and capability in order to identify system drivers.

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