The background and development status of an ultralightweight flexible-blanket flatpack, fold-out solar array is presented. It is scheduled for prototype demonstration in late 1989. The Advanced Photovoltaic Solar Array (APSA) design represents a critical intermediate milestone of the goal of 300 W/kg at beginning-of-life (BOL) with specific performance characteristics of 130 W/kg (BOL) and 100 W/kg at end-of-life (EOL) for a 10-year geosynchronous geostationary earth orbit 10-kW (BOL) space power system. The APSA wing design is scalable over a power range of 2 to 15 kW and is suitable for a full range of missions including Low Earth Orbit (LEO), orbital transfer from LEO to geostationary earth orbit and interplanetary flight.


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    Titel :

    The advanced photovoltaic solar array program


    Beteiligte:
    Kurland, R. M. (Autor:in) / Stella, Paul M. (Autor:in)


    Erscheinungsdatum :

    01.08.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Advanced Photovoltaic Solar Array Program status

    Kurland, R.M. / Stella, P.M. | Tema Archiv | 1989


    Advanced photovoltaic solar array design

    Kurland, R. / Stella, P. | Tema Archiv | 1987


    Advanced photovoltaic solar array - Design and performance

    KURLAND, RICHARD / STELLA, PAUL | AIAA | 1992


    Operational Considerations of the Advanced Photovoltaic Solar Array

    Stella, Paul M. / Kurland, Richard M. | SAE Technical Papers | 1992