A detailed Neptune aerocapture systems analysis and spacecraft design study was performed as part of NASA's In-Space Propulsion Program. The primary objectives were to assess the feasibility of a spacecraft point design for a Neptune/Triton science mission. That uses aerocapture as the Neptune orbit insertion mechanism. This paper provides an overview of the science, mission and spacecraft design resulting from that study.


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    Titel :

    Neptune aerocapture mission and spacecraft design overview


    Beteiligte:
    Bailey, Robert W. (Autor:in) / Hall, Jeff L. (Autor:in) / Spliker, Tom R. (Autor:in) / O'Kongo, Nora (Autor:in)

    Kongress:

    40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 2004 ; Fort Lauderdale, FL, United States


    Erscheinungsdatum :

    12.07.2004


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Structural Design for a Neptune Aerocapture Mission

    R. E. Dyke / G. A. Hrinda | NTIS | 2004


    Titan aerocapture mission and spacecraft design overview

    Bailey, R. W. / Hall, J. L. / Spilker, T. R. | NTRS | 2003


    TITAN AEROCAPTURE MISSION AND SPACECRAFT DESIGN OVERVIEW

    Bailey, R. W. / Hall, J. L. / Spilker, T. R. et al. | British Library Conference Proceedings | 2003