Dependence of solar array energy on orbital parameters is given for cases that achieve optimum array pointing and maximum performance; optimum pointing requires continual array articulation and/or active spacecraft attitude control; performance obtained in local-vertical attitudes with fixed or incrementally articulated arrays is compared with maximum. (30798)


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    Titel :

    Solar array performance as function of orbital parameters and spacecraft attitude


    Weitere Titelangaben:

    ASME Aviation Space -- Progress Prospects


    Beteiligte:
    Hough, W.W. (Autor:in) / Elrod, B.D. (Autor:in)

    Kongress:

    ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Power supply



    Erscheinungsdatum :

    1968


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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