The Mars Atmosphere and Volatile Evolution (MAVEN) mission will determine the history of the loss of volatiles from the Martian atmosphere from a highly inclined elliptical orbit. MAVEN will launch from Cape Canaveral Air Force Station on an Atlas-V 401 during an extended 36-day launch period opening November 18, 2013. The MAVEN Navigation and Mission Design team performed a Monte Carlo analysis of the Type-II transfer to characterize; dispersions of the arrival B-Plane, trajectory correction maneuvers (TCMs), and the probability of Mars impact. This paper presents detailed analysis of critical MOI event coverage, maneuver constraints, deltaV-99 budgets, and Planetary Protection requirements.


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    Title :

    Transfer Trajectory Design for the Mars Atmosphere and Volatile Evolution (MAVEN) Mission


    Contributors:
    Folta, David (author) / Demcak, Stuart (author) / Young, Brian (author) / Berry, Kevin (author)

    Conference:

    AAS/AIAA Spaceflight Mechanics Meeting ; 2013 ; Kauai, HI, United States


    Publication date :

    2013-02-10


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English