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Accretional capture of the moonThe effectiveness of accretional capture is studied with the aid of a simple model involving a small secondary body in a hyperbolic orbit which approaches a large primary body. When the separation is a minimum, the mass of the primary body increases. An investigation is conducted regarding the conditions under which this change in mass will result in an elliptic orbit with capture.
Document ID
19760031202
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Clark, S. P., Jr.
(Yale University New Haven, Conn., United States)
Turcotte, D. L.
(Cornell Univ. Ithaca, NY, United States)
Nordmann, J. C.
(Cornell University Ithaca, N.Y., United States)
Date Acquired
August 8, 2013
Publication Date
November 20, 1975
Publication Information
Publication: Nature
Volume: 258
Subject Category
Lunar And Planetary Exploration
Accession Number
76A14168
Funding Number(s)
CONTRACT_GRANT: NGR-33-010-108
Distribution Limits
Public
Copyright
Other

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