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Long term behavior of artificial satellite orbits due to third-body perturbations.Long term time-variation of osculating elements of satellite orbits perturbed by third body, including graphs of Kepler element variations along different orbits
Document ID
19660050927
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lorell, J.
Date Acquired
August 3, 2013
Publication Date
December 1, 1965
Publication Information
Publication: JOURNAL OF THE ASTRONAUTICAL SCIENCES
Subject Category
Space Sciences
Accession Number
66A30217
Distribution Limits
Public
Copyright
Other
Keywords
SATELLITE PERTURBATION
ORBIT PERTURBATION

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