Recent trades have taken place on solid propulsion options to support a potential Mars Sample Retrieval Campaign. Mass and dimensional requirements for a Mars Ascent Vehicle (MAV) are being assessed. One MAV vehicle concept would utilize a solid propulsion system. Key challenges to designing a solid propulsion system for MAV include low temperatures beyond common tactical and space requirements, performance, planetary protection, mass limits, and thrust vector control system. Two solutions are addressed, a modified commercial commercially available system, and an optimum new concept.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Mars Ascent Vehicle (MAV) Solid Motor Technology Plans


    Beteiligte:
    Prince, Andrew (Autor:in) / McCauley, Rachel (Autor:in) / Kibbey, Timothy (Autor:in) / McCollum, Lisa (Autor:in) / Oglesby, Britt (Autor:in) / Stefanski, Philip (Autor:in)

    Kongress:

    IEEE Aerospace Conference ; 2019 ; Big Sky, MT, United States


    Erscheinungsdatum :

    2019-03-02


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mars Ascent Vehicle Propulsion System Solid Motor Technology Plans

    Prince, Andrew / McCauley, Rachel / Kibbey, Timothy et al. | NTRS | 2019


    Mars Ascent Vehicle-First Stage Motor

    Dankanich, John / Doudrick, Scott / Williams, Jacob | NTRS | 2015


    Mars Ascent Vehicle technology planning

    Dankanich, John W. | IEEE | 2009