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.


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    Title :

    Flight path control strategies and preliminary deltaV requirements for the 2007 Mars Phoenix (PHX) mission


    Contributors:

    Conference:

    AAS/AIAA Astrodynamics Specialist Conference ; 2005 ; Lake Tahoe, CA, United States


    Publication date :

    2005-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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