This paper will cover the conceptual design of a Mars Ascent Vehicle (MAV) and efforts underway to raise the TRL at both the component and system levels. A system down select was executed resulting in a Hybrid Propulsion based Single Stage To Orbit (SSTO) MAV baseline architecture. This paper covers the Point of Departure design, as well as results of hardware developments that will be tested in several upcoming flight opportunities.


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    Titel :

    A Mars Ascent Vehicle for potential mars sample return


    Beteiligte:
    Shotwell, Robert (Autor:in) / Benito, Joel (Autor:in) / Karp, Ashley (Autor:in) / Dankanich, John (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.03.2017


    Format / Umfang :

    5945049 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    A Mars Ascent Vehicle for Potential Mars Sample Return

    Shotwell, Robert / Benito, Joel / Karp, Ashley et al. | NTRS | 2017


    A Mars Ascent Vehicle for Potential Mars Sample Return

    Dankanich, John / Karp, Ashley / Benito, Joel et al. | NTRS | 2017


    Mars Sample Return Mission: Mars Ascent Vehicle Propulsion Design

    Sopegno, Laura / Valavanis, Kimon P. / Rutherford, Matthew J. et al. | IEEE | 2020


    Mars Sample Return Mission: Mars Ascent Vehicle Propulsion Design

    Sopegno L. / Valavanis K. P. / Rutherford M. J. et al. | BASE | 2020

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