This paper describes the design and component testing of an aerobot that would be capable of global in situ exploration of Saturn's moon, Titan, over a 6 to 12 month mission lifetime. The proposed aerobot is a propeller-driven, buoyant vehicle that resembles terrestrial airships. However, the extremely cold Titan environment requires the use of cryogenic materials of construction and careful thermal design for protection of temperature-sensitive payload elements. Multiple candidate balloon materials have been identified based on extensive laboratory testing at 77 K.


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    Titel :

    An aerobot for global in situ exploration of Titan


    Beteiligte:
    Hall, J. L. (Autor:in) / Kerzhanovich, V. V. (Autor:in) / Yavrouian, A. H. (Autor:in) / Jones, J. A. (Autor:in) / White, C. V. (Autor:in) / Dudik, B. A. (Autor:in) / Plett, G. A. (Autor:in) / Mennella, J. (Autor:in) / Elfes, A. (Autor:in)

    Kongress:

    35th Committee on Space Research (COSPAR) Scientific Assembly ; 2004 ; Paris, France


    Erscheinungsdatum :

    2004-07-18


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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