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    Conceptual design of the Mars Rover Sample Return system (1989)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: AIAA PAPER 89-0418
    Format: text
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