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Low-thrust, minimum-fuel, orbital transfersLow thrust minimum fuel space vehicle transfer from initial circular orbit to coplanar elliptic orbit of given energy and angular momentum
Document ID
19710043637
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Brusch, R. G.
Vincent, T. L.
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Subject Category
Space Sciences
Accession Number
71A24334
Funding Number(s)
CONTRACT_GRANT: NGR-03-002-011
Distribution Limits
Public
Copyright
Other

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