Mass, area, and station-keeping propellant needs have been estimated for a typical system. And, although important criteria such as cost, Shuttle packaging, and erection/deployment schemes were not considered, the documented trends should aid in many of the design choices to be made. Effects on system characteristics were examined for: three heat storage salts with melting temperatures from 743 to 1121 K; parabolic and Cassegrainian mirrors; module power levels of 20 and 40 kW; and, alternate pumped-loop, tube-and-fin radiator configurations, with and without micrometeoroid armoring.


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    Titel :

    Design tradeoffs for a space station solar-Brayton power system


    Weitere Titelangaben:

    Rahmenbedingungen fuer die Planung eines solaren Brayton-Energieversorgungssystems fuer die Raumstation


    Beteiligte:
    Klann, J.L. (Autor:in) / Staiger, P.J. (Autor:in)


    Erscheinungsdatum :

    1985


    Format / Umfang :

    14 Seiten, 22 Bilder, 10 Tabellen, 7 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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