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Two fixed center approximations to the restricted problem.Earth moon trajectory is considered by using perturbation theory in three-body problem for case of two fixed centers
Document ID
19640040302
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Payne, M.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-390
Report Number: AIAA PAPER 63-390
Accession Number
64A26195
Funding Number(s)
CONTRACT_GRANT: NAS8-2605
Distribution Limits
Public
Copyright
Other
Keywords
THREE-BODY PROBLEM

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