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Mars Reconnaissance Orbiter: aerobraking reference trajectoryThis paper describes the aerobraking baseline trajectory that formed the basis of the reference mission presented at the Mars Reconnaissance Orbiter Preliminary Design Review.
Document ID
20060029684
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/8855
Authors
Lyons, D. T.
Date Acquired
August 23, 2013
Publication Date
August 5, 2002
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Other
Keywords
aerobraking Mars Orbiter

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