NASA NTRS · 19890037979
Conceptual design of the Mars Rover Sample Return system
Abstract
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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Rose, James R.. 1989-01-01. Conceptual design of the Mars Rover Sample Return system. https://ntrs.nasa.gov/citations/19890037979
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