This paper addresses critical issues for implementation of the technology, mission design constraints, configuration concepts and overall performance characteristics, including results of aerothermal and aerostability analyses, guidance algorithm design and performance, and overall system characteristics. The effort to date has focused on capture at Mars and Titan.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Trailing Ballute Aerocapture : concept and feasibility assessment


    Beteiligte:
    Wilmoth, Richard G. (Autor:in) / Lyons, Daniel T. (Autor:in) / Stein, Jim (Autor:in) / Trochman, Bill (Autor:in) / Miller, Kevin L. (Autor:in) / Lewis, Jake (Autor:in)

    Erscheinungsdatum :

    2003-07-20


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Trailing Ballute Aerocapture: Concept and Feasibility Assessment

    K. L. Miller / D. Gulick / J. Lewis et al. | NTIS | 2003


    Trailing Ballute Aerocapture: Concept and Feasibility Assessment

    Miller, Kevin L. / Gulick, Doug / Lewis, Jake et al. | NTRS | 2003


    Trailing Ballute Aerocapture: System Definition

    Gulick, Douglas / Lewis, Jackson / Miller, Kevin et al. | AIAA | 2003



    Ballute Aerocapture Trajectories at Neptune

    Lyons, Daniel T. / Johnson, Wyatt | NTRS | 2004