The military spacecraft power subsystem design requirements, developments goals, and planned technology efforts are summarized. The mission drivers of performance (weight and volume), hardening (survivability), autonomy, reliability, and miniaturization influence space mission effectiveness are outlined. The anticipated performance versus power level trends for reactor static conversion systems are illustrated. A conceptual design for a space based radar system is also given.


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    Titel :

    Air Force space power technology program


    Beteiligte:
    Barthelemy, R. (Autor:in) / Mahefkey, T. (Autor:in) / Hebblewaite, T. (Autor:in)


    Erscheinungsdatum :

    1980-09-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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