Planetary Missions from GTO Using Earth and Moon Gravity Assists

Penzo, P. A.

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