The Insat-1 satellite will provide a significant development in solar ray technology for synchronous orbit high power satellites. It is a three-axis stabilized spacecraft designed for seven year operation to provide communications/meteorological service to India. Primary energy source is a single-axis, single-tracking solar array wing with solar torque offset by an opposing solar sail boom. The solar array, composed of five graphite epoxy rigid deployable panels, provides 1000 W divided between two separate power buses.


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    Titel :

    Design Summary of the Insat Lightweight, Deployable Solar Array


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Dixson, J. (Autor:in) / Barberis, N. J. (Autor:in) / Woytowitz, P. (Autor:in)

    Kongress:

    Aerospace Congress and Exposition ; 1982



    Erscheinungsdatum :

    01.02.1982




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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