This paper describes the methods used to estimate the statistical deltaV requirements for the propulsive maneuvers that will deliver the spacecraft to its target landing site while satisfying planetary protection requirements. the paper presents flight path control analysis results for three different trajectories, open, middle, and close of launch period for the mission.
Flight path control strategies and preliminary deltaV requirements for the 2007 Mars Phoenix (PHX) mission
AAS/AIAA Astrodynamics Specialist Conference ; 2005 ; Lake Tahoe, CA, United States
2005-08-01
Conference paper
No indication
English
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