Types of space mission and velocity increments required; nuclear rocket applications are divided into missions which start from Earth's surface and require thrusts greater than vehicle takeoff weight, and missions which start from satellite orbit about Earth requiring thrusts only small fraction of starting weight; particular consideration given to low power space nuclear rocket concept and estimated performance.


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    Titel :

    Nuclear rockets for interplanetary propulsion


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Rom, F.E. (Autor:in) / Johnson, P.G. (Autor:in)

    Kongress:

    SAE Meeting ; 1959 Nuclear



    Erscheinungsdatum :

    1959


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Rom, F.E. / Johnson, P.G. | Engineering Index Backfile | 1960


    Mechanics of interplanetary rockets

    Senftleben, H.A. | Engineering Index Backfile | 1928


    Rockets and Interplanetary Flights

    B. V. Lyapunov | NTIS | 1963


    Perigee propulsion for orbital launch of nuclear rockets

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