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Recent developments in analytical celestial mechanicsDerivation of closed perturbed precessing elliptic orbits of arbitrary eccentricity and small major axis about smaller of two attracting bodies of arbitrary mass ratio
Document ID
19660018019
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Arenstorf, R. F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Accession Number
66N27309
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CELESTIAL MECHANICS
KEPLER LAW
THREE-BODY PROBLEM
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