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2001 Mars Odyssey aerobrakingThe 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.
Document ID
20060029653
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/8817
Authors
Smith, J. C.
Bell, J. L.
Date Acquired
August 23, 2013
Publication Date
August 5, 2002
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
Mars Odyssey aerobraking mission design navigation

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