Cloud Cover Satellite flown in Vanguard vehicles SLV-3 and SLV-4 required spin rate of 55 rpm when entering orbit; although required spin-reduction mechanism functioned properly, desired spin rate was not achieved owing to uncontrollable flight effects; to meet future requirements control system is needed which can orient payload according to predetermined scheme and maintain it for desired period.


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    Titel :

    Vanguard Satellite spin-reduction mechanism


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Baumann, R.C. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Vanguard satellite spin-reduction mechanism

    Baumann, Robert C. | TIBKAT | 1961


    Vanguard Satellite Spin-Reduction Mechanism

    Baumann, Robert C. | NTRS | 1961



    Vanguard satellite

    Furnas, C.C. | Engineering Index Backfile | 1957


    Vanguard I Satellite Structure and Separation Mechanism

    Shea, John T. / Baumann, Robert C. | NTRS | 1961