The presented trajectory design and analysis was performed for the Phobos and Deimos & Mars Environment (PADME) mission concept as part of a NASA proposal submission managed by NASA Ames Research Center in the 2014-2015 timeframe. The PADME spacecraft would be a derivative of the successfully flown Lunar Atmosphere & Dust Environment Explorer (LADEE) spacecraft. While LADEE was designed to enter low-lunar orbit, the PADME spacecraft would instead enter an elliptical Mars orbit of 2-week period. This Mars orbit would pass by Phobos near periapsis on successive orbits and then raise periapsis to yield close approaches of Deimos every orbit thereafter.


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    Titel :

    Trajectory Design for the Phobos and Deimos & Mars Environment Spacecraft


    Beteiligte:
    A. L. Genova (Autor:in) / D. J. Korsmeyer (Autor:in) / M. E. Loucks (Autor:in) / F. Y. Yang (Autor:in) / P. Lee (Autor:in)

    Erscheinungsdatum :

    2016


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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