Synchronous gravity-stabilized advanced technology satellite (ATS) is described; it is designed to be despun by two-stage yo-yo in combination with nutation damper; unique advantage of ATS despin mechanism arises from use of two-stage yo-yo system in which off-axis rate errors of first stage, starting from 100 rpm, are damped out by nutation damper prior to releasing second-stage yo-yo, starting from 10 rpm.


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    Titel :

    Despinning ATS satellite


    Weitere Titelangaben:

    Aerospace Mechanisms Symposium -- Proc


    Beteiligte:
    Dallas, J.P. (Autor:in)

    Kongress:

    2nd Aerospace Mechanisms Symposium ; 1967 ; United States , Pasadena, CA Stability



    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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