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Two-center problem orbits as intermediate orbits for the restricted three-body problemTwo-center problem orbit as intermediate orbit for restricted three-body problem
Document ID
19650022582
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Langebartel, R. G. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-2939
Report Number: NASA-TN-D-2939
Accession Number
65N32183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CELESTIAL MECHANICS
THREE-BODY PROBLEM
PROBLEM SOLVING

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