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Mars sample-return optionsAttention is given to the comparative merits of two options for the return to earth of Mars round-trip sampling probe missions. The first option makes use of an onboard propulsion system to place the returning vehicle into a highly elliptical orbit around the earth. An orbital transfer vehicle (OTV) or OTV/orbital maneuvering vehicle combination retrieves the sample from the return vehicle. The second option uses aerocapture to place the return vehicle in earth orbit; this maneuver imposes no greater weight penalty for proceeding to a low orbit than remaining at one that is high. The second option delivers the sample to a Space Station-compatible orbit for pickup.
Document ID
19860029509
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
French, J. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Norton, H. N.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Klein, G. A.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1985
Publication Information
Publication: Aerospace America
Volume: 23
ISSN: 0740-722X
Subject Category
Lunar And Planetary Exploration
Accession Number
86A14247
Distribution Limits
Public
Copyright
Other

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