Charts are presented of weight as function of thrust, specific impulse, initial weight in orbit, and mission energy for orbital-launch nuclear rockets; initial weights range from 7600 to 226,000 lb (corresponding to Atlas-Centaur, Saturn, and Nova boost vehicles), and missions are selected to cover approximate capability inherent in specified weights.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Residual-load-plus-powerplant weights for orbital-launch nuclear rockets


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Johnson, P.G. (Autor:in) / Miser, J.W. (Autor:in) / Smith, R.L. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Residual-load-plus-powerplant weights for orbital-launch nuclear rockets

    Johnson, Paul G. / Miser, James W. / Smith, Roger L. | TIBKAT | 1961



    Perigee propulsion for orbital launch of nuclear rockets

    Johnson, Paul G. ;Rom, Frank E. | SLUB | 1962


    Perigee propulsion for orbital launch of nuclear rockets

    Johnson, Paul G. / Rom, Frank E. | TIBKAT | 1962


    PERIGEE PROPULSION FOR ORBITAL LAUNCH OF NUCLEAR ROCKETS

    Johnson, P. G. / Rom, F. E. | NTRS | 1962