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Trajectory design for the Mars Reconnaissance Orbiter mission
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Trajectory design for the Mars Reconnaissance Orbiter mission
Halsell, C. A.
;
Bowes, A. L.
;
Johnston, M. D.
;
Lyons, D. T.
;
Lock, R. E.
;
Xaypraseuth, P.
;
Bhaskaran, S.
;
Highsmith, D. E.
;
Jah, M. K.
URI:
http://hdl.handle.net/2014/6542
Date:
2003-02-10
Citation:
13th AAA/AISS Space Flight Mechanics Meeting
Ponce, Puerto Rico
Abstract:
This paper describes the analysis and design evolution of the Mars Reconnaissance Orbiter trajectory from launch to end-of-mission.
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JPL TRS 1992+
JPL TRS 1992+
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