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Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.Payload capabilities of low thrust power limited spacecraft for earth to mars round trip trajectories
Document ID
19640041237
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Melbourne, W. G.
Sauer, C. G., Jr.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Space Radiation
Accession Number
64A27130
Distribution Limits
Public
Copyright
Other
Keywords
ORBITAL TRANSFER
ROUND-TRIP TRAJECTORY
SPACECRAFT TRAJECTORY

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