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Mars Ascent Propulsion on a Minimum Scale
A concept is presented for a single stage vehicle intended to lift a Mars sample to an orbital rendezvous.
Document ID
20210005424
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/19161
Authors
Guernsey, C.
Whitehead, J. C.
Date Acquired
April 27, 1998
Publication Date
April 27, 1998
Publication Information
Publisher:
UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Mars
orbital
rendezvous
single
stage
sample
return
Mars
ascent
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