A roll-out flexible array which provides more than 4 kW of power for the space telescope was developed. The Array is configured as two wings. The deployment mechanism for each wing is based on flight-proven FRUSA design. Modifications have been incorporated to accommodate an increase in size and mission requirements. The assembly and operation of the deployment mechanism are described together with environmental and functional tests results.


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    Titel :

    A deployment mechanism for the double roll-out flexible solar array on the space telescope


    Beteiligte:
    Cawsey, T. R. (Autor:in)


    Erscheinungsdatum :

    01.05.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The double roll-out solar array for space telescope

    Crabb, R.L. / Williams, C.J. | Tema Archiv | 1978


    Solar Array Deployment Mechanism

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    FLEXIBLE SOLAR ARRAY FOR EXTRATERRESTRIAL DEPLOYMENT

    KRUER MARK A / YAMANE JUD J | Europäisches Patentamt | 2022

    Freier Zugriff