Study of conceptual power plant design indicates that radiator necessary for rejecting cycle waste heat is dominant weight; thermodynamic cycle using sodium vapor as working fluid and operating at turbine-inlet temperature of 2500 R is selected to reduce weight; total power plant weight is approximately 6 lb per kw.


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    Titel :

    20,000-kilowatt nuclear turboelectric power supply for manned space vehicles


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    English, R.E. (Autor:in) / Slone, H.O. (Autor:in) / Bernatowicz, D.T. (Autor:in) / Davison, E.H. (Autor:in) / Lieblein, S. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    65 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Turboelectric Power Generation for Space Vehicles

    Ross, Daniel P. / Taylor, J. Edward | SAE Technical Papers | 1961


    SNAP 2 A Reactor Powered Turboelectric Generator for Space Vehicles

    Anderson, Lt. Col. Guveren M. | SAE Technical Papers | 1961