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A model for close encounters in the planetary problemA model is proposed for single close encounters between two small masses, m1 and m2, which orbit a much larger mass, M. The main new feature of the model is the assumption of conic motion of the center of mass of m1 and m2 in the gravitational field of M. Comparisons of the model with the three-body equations of motion indicate that the model is a useful approximation for m1, m2 not exceeding 0.00001 M. The model is therefore applicable for encounters between bodies of the order of an earth mass or smaller in the presence of the sun. Comparisons are also made of outcomes obtained by the model with outcomes of numerical integration for a large variety of close encounters. The above comparisons reveal that for many purposes the model is an adequate approximation for encounters with an eccentricity of the hyperbolic orbit of m1 about m2 not less than 4.
Document ID
19780054430
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cox, L. P.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Lewis, J. S.
(MIT Cambridge, Mass., United States)
Lecar, M.
(Harvard College Observatory and Smithsonian Astrophysical Observatory, Center for Astrophysics, Cambridge Mass., United States)
Date Acquired
August 9, 2013
Publication Date
May 1, 1978
Publication Information
Publication: Icarus
Volume: 34
Subject Category
Lunar And Planetary Exploration
Accession Number
78A38339
Funding Number(s)
CONTRACT_GRANT: NGL-22-009-521
Distribution Limits
Public
Copyright
Other

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