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 |