Gas-cycle nuclear-rocket power plants with hydrogen as propellant are considered as propulsion devices for space vehicles; summary of analysis conducted over range of reactor power of 46 to 1600 Mw; analysis of local heat-flux capability of coolant at nozzle throat indicated that cooling capability was inadequate to maintain wall temperature of 1440 R; techniques for improving capability such as h-p drop, high wall temperature, refractory wall coatings, etc.


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    Titel :

    Analysis of nuclear-rocket nozzle cooling


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Robbins, W.H. (Autor:in) / Bachkin, D. (Autor:in) / Medeiros, A.A. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    An analysis of nuclear-rocket nozzle cooling

    Robbins, William H. / Bachkin, Daniel / Medeiros, Arthur A. | TIBKAT | 1960



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