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ORBITAL RENDEZVOUS CONSIDERATIONS FOR A MARS MISSIONOrbital rendezvous considerations for mars mission requiring tangential approach to, and departure from, orbit to achieve maximum propulsive efficiency
Document ID
19630028696
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bird, J. D.
Thomas, D. F.
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Space Radiation
Accession Number
63A24755
Distribution Limits
Public
Copyright
Other
Keywords
RENDEZVOUS TRAJECTORY
MARS /PLANET/
ORBITAL RENDEZVOUS

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