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Mars sample return missions, precursors to manned planetary explorationTechnologies and concepts applicable to eventual manned exploration of Mars, as demonstrated by the Mars Sample Return Mission, are presented. These include aerocapturing at Mars; safe and accurate descent and landing effectively using aerobraking and propulsion; launch and ascent from the Martian surface; rendezvous and docking with an orbiting return vehicle; and a safe return to earth. Critical mission elements are expected to function independently of either earth or astronaut control to ensure human safety. The Mars Rover Sample Return Mission includes such elements as autonomous functions in this unmanned mission. Based on the analyses performed and the concepts investigated, it is suggested that robotic missions are feasible for late 1990s without any major technology development being required.
Document ID
19910029397
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stager, D. N.
(TRW, Inc. Redondo Beach, CA, United States)
Cruz, M. I.
(TRW, Inc. Redondo Beach, CA, United States)
Balmanno, W. F.
(TRW, Inc. Redondo Beach, CA, United States)
Hieatt, J. L.
(TRW, Inc. Federal Systems Div., Redondo Beach, CA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Subject Category
Astronautics (General)
Report/Patent Number
IAF PAPER 90-417
Accession Number
91A14020
Funding Number(s)
CONTRACT_GRANT: NAS9-18141
Distribution Limits
Public
Copyright
Other

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