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Contributions to the elliptic restricted three- body problem.Elliptic restricted three-body problem solved for eigenvalues and orbital series solutions of Lagrangian triangular point
Document ID
19670042485
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lanzano, P.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Publication Information
Publication: ICARUS
Subject Category
Space Sciences
Accession Number
67A21214
Funding Number(s)
CONTRACT_GRANT: NASW-1309
Distribution Limits
Public
Copyright
Other
Keywords
ORBITAL CALCULATION
THREE-BODY PROBLEM

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