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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Air Force space power technology program


    Contributors:


    Publication date :

    1980-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    The NASA space power technology program

    Landingham, E.E. van | Tema Archive | 1986


    The NASA space power technology program

    Mullin, J. P. | NTRS | 1978


    The NASA space power technology program

    Vanlandingham, E. E. | NTRS | 1986


    The NASA space power technology program

    Mullin, J.P. / Hudson, W.R. / Randolf, L.P. | Tema Archive | 1979