In NASA's evolvable Mars campaign, transportation architectures for human missions to Mars rely on a combination of solar electric propulsion and chemical propulsion systems. Minimizing the Mars ascent vehicle (MAV) mass is critical in reducing the overall lander mass and also eases the requirements placed on the transportation stages. This paper presents the results of a conceptual design study to obtain a minimal MAV configuration, including subsystem designs and mass summaries.


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    Titel :

    Mars Ascent Vehicle Design for Human Exploration


    Beteiligte:
    Polsgrove, Tara (Autor:in) / Thomas, Dan (Autor:in) / Sutherlin, Steven (Autor:in) / Stephens, Walter (Autor:in) / Rucker, Michelle (Autor:in)

    Kongress:

    AIAA SPACE 2015 ; 2015 ; Pasadena, CA, United States


    Erscheinungsdatum :

    2015-08-31


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Mars Ascent Vehicle Design for Human Exploration

    Polsgrove, Tara / Thomas, Herbert D. / Stephens, Walter et al. | AIAA | 2015


    Update to Mars Ascent Vehicle Design for Human Exploration

    T. P. Polsgrove / T. K. Percy / M. Rucker et al. | NTIS | 2019


    Update to Mars Ascent Vehicle Design for Human Exploration

    Polsgrove, Tara P. / Percy, Thomas K. / Rucker, Michelle et al. | NTRS | 2019


    Mars Ascent Vehicle Design for Human Exploration (AIAA 2015-4416)

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