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  • 1
    Publication Date: 2019-06-27
    Description: The 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.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: Nature; 258; Nov. 20
    Format: text
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