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Planetary Missions from GTO Using Earth and Moon Gravity Assists
A general method has been developed which permits the transfer of a spacecraft from a highly elliptic and generally oriented Earth orbit to a specified escape direction and energy.
Document ID
20060041325
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/19526
Authors
Penzo, P. A.
Date Acquired
August 23, 2013
Publication Date
August 10, 1998
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
planetary missions GTO moon gravity earth gravity
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