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SINGULAR EXTREMALS IN LAWDEN'S PROBLEM OF OPTIMAL ROCKET FLIGHTOptimal rocket flight in gravitational field using lawdens results on intermediate thrust subarcs
Document ID
19630023362
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kelly, H. J.
Date Acquired
August 1, 2013
Publication Date
July 1, 1963
Subject Category
Space Sciences
Accession Number
63A19421
Funding Number(s)
CONTRACT_GRANT: AF 29/600/-2671
CONTRACT_GRANT: NAS8-1549
Distribution Limits
Public
Copyright
Other
Keywords
ROCKET FLIGHT
GRAVITATIONAL EFFECT

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