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An optimal, analytic solution to the linear- gravity, constant-thrust trajectory problemConstant-thrust trajectory problem with gravitational acceleration as linear function of radius vector, obtaining minimum fuel solution in integrals
Document ID
19710051346
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jezewski, D. J.
Date Acquired
August 6, 2013
Publication Date
July 1, 1971
Subject Category
Space Sciences
Accession Number
71A32043
Distribution Limits
Public
Copyright
Other

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