Examines the potential of dual-purposing an ascent vehicle for both Moon and Mars missions. Finds similarities in V, thrust, crew cabin, and power/thermal subsystem requirements. Tighter mass budgets for Mars vs. Moon mission. Potential challenges that need more detailed design and analysis to answer.


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    Titel :

    A Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy


    Beteiligte:
    Timothy Lewis (Autor:in) / Emily Judd (Autor:in) / Zachary May (Autor:in) / Ryan Joyce (Autor:in)

    Kongress:

    ASCEND ; 2020 ; Virtual, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy

    T. Lewis / E. Judd / Z. May et al. | NTIS | 2020


    Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy

    T. A. Lewis / E. L. Judd / Z. D. May et al. | NTIS | 2020


    A Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy

    Timothy A Lewis / Emily L Judd / Zachary D May et al. | NTRS


    A Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy

    Lewis, Timothy A. / Judd, Emily / Joyce, Ryan T. et al. | AIAA | 2020