Technology development to mature a hybrid rocket option for a potential Mars Ascent Vehicle has been underway at the Jet Propulsion Laboratory and Marshall Space Flight Center. A conceptual design was completed in 2016 and has been used to determine the motor size for risk reduction development. The task plan for the FY17 testing, actually completed in mid FY18, is discussed. The major achievement of this effort was successful full scale hotfire testing with a representative ambient Earth storable propellant combination: SP7/MON3. A near term plan, through July 2019 is briefly discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept


    Beteiligte:
    Prince, Andrew (Autor:in) / Oglesby, Britt (Autor:in) / Story, George (Autor:in) / Vaughan, David (Autor:in) / Nakazono, Barry (Autor:in) / Karp, Ashley C. (Autor:in)

    Erscheinungsdatum :

    2018-07-09


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept

    Prince, Andrew / Oglesby, Britt / Story, George et al. | NTRS | 2018


    Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept

    Karp, Ashley C. / Nakazono, Barry / Vaughan, David A. et al. | AIAA | 2018


    Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept (AIAA 2018-4834)

    Karp, Ashley C. / Nakazono, Barry / Vaughan, David A. et al. | British Library Conference Proceedings | 2018



    Technology Development Plan and Preliminary Results for a Low Temperature Hybrid Mars Ascent Vehicle Concept

    Karp, Ashley C. / Nakazono, Barry / Shotwell, Robert et al. | AIAA | 2017