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Planetary Missions from GTO Using Earth and Moon Gravity Assists

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dc.contributor.author Penzo, P. A. en_US
dc.date.accessioned 2004-09-24T21:06:00Z
dc.date.available 2004-09-24T21:06:00Z
dc.date.issued 1998-08-10 en_US
dc.identifier.citation AIAA Astrodynamics Specialist Conference en_US
dc.identifier.citation Boston, MA, USA en_US
dc.identifier.clearanceno 98-0946 en_US
dc.identifier.uri http://hdl.handle.net/2014/19526
dc.description.abstract 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. en_US
dc.format.extent 621434 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other planetary missions GTO moon gravity earth gravity en_US
dc.title Planetary Missions from GTO Using Earth and Moon Gravity Assists en_US


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