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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Parametric Assessment of Lunar and Mars Ascent Vehicle Synergy


    Beteiligte:
    T. Lewis (Autor:in) / E. Judd (Autor:in) / Z. May (Autor:in) / R. Joyce (Autor:in)

    Erscheinungsdatum :

    2020


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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 Lewis / Emily Judd / Zachary May et al. | NTRS


    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