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A simple linear approximation for perturbed motion about moderately elliptic orbits
Moderately elliptic reference orbit perturbed motion, applying linearized perturbation equations for circular orbit
Document ID
19700068474
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Koble, H. M.
Schneider, A. M.
Date Acquired
August 5, 2013
Publication Date
October 1, 1970
Subject Category
Space Sciences
Accession Number
70A44590
Funding Number(s)
CONTRACT_GRANT: NGR-05-009-106
Distribution Limits
Public
Copyright
Other
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