This paper describes the methods used to estimate the statistical delta V and propellant requirements for propulsive maneuvers necessary to deliver the two Rovers while ensuring that planetary protection requirements are satisfied.
Flight path control strategies for the 2003 Mars Exploration Rover (MER) mission
AIAA/AAS Astrodynamics Specialist Conference
2002-08-05
Conference paper
No indication
English
AIAA-2002-4824 Flight Path Control Strategies for the 2003 Mars Exploration Rover (MER) Mission
British Library Conference Proceedings | 2002
|AIAA-2002-4824 Flight Path Control Strategies for the 2003 Mars Exploration Rover (MER) Mission
British Library Conference Proceedings | 2002
|Mars Exploration Rover Mission
NTRS | 2008
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