An innovative concept is proposed for atmospheric entry probe deceleration, wherein one or more deployed rotors (in autorotation or wind-turbine flow states) on the aft end of the probe effect controlled descent. This concept is particularly oriented toward probes intended to land safely on the surface of Venus. Initial work on design trade studies is discussed.


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    Titel :

    Rotary-Wing Decelerators for Probe Descent Through the Atmosphere of Venus


    Beteiligte:
    Young, Larry A. (Autor:in) / Briggs, Geoffrey (Autor:in) / Aiken, Edwin (Autor:in) / Pisanich, Greg (Autor:in)


    Erscheinungsdatum :

    01.04.2005


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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