The Mars Odyssey spacecraft was inserted into a highly elliptical capture orbit about Mars on October 24, 2001. This paper details the strategy, implementation, and results of the aerobraking phase of the mission.
2001 Mars Odyssey aerobraking
AIAA/AAS Astrodynamics Conference
2002-08-05
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2005
|AIAA | 2005
|AIAA | 2002
|SPECIAL SECTION: 2001 MARS ODYSSEY MISSION - 2001 Mars Odyssey Aerobraking
Online Contents | 2005
|AIAA-2002-4532 2001 Mars Odyssey Aerobraking
British Library Conference Proceedings | 2002
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