A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy turbo pumps in a conventional rocket engine. The substitution results in a substantial reduction in rocket engine weight. The flame emanating from the small rocket motor can act to ignite non-hypergolic fuels.


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    Title :

    Supersonic-Combustion Rocket


    Contributors:

    Publication date :

    1973


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Supersonic-combustion rocket

    Weber, R. J. / Franciscus, L. C. | NTRS | 1973





    Supersonic Rocket Launcher

    E. P. Lowe / R. D. Stubbs | NTIS | 1975