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