The patent relates to a combination rocket motor ramjet engine having the rocket motor located in the ramjet inlet diffuser. All or part of the rocket portion of the apparatus remaining after rocket booster burnout are ejected by air pressure in the diffuser inlet to permit the diffuser to supply ram air for the ramjet engine.


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    Title :

    Ramjet with Integrated Rocket Boost Motor


    Contributors:

    Publication date :

    1974


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Ramjet with Integrated Rocket Boost Motor

    J. H. Leingang | NTIS | 1974


    Ramjet with Integrated Rocket Boost Motor

    J. L. Leingang | NTIS | 1972




    British Rocket and Ramjet Engines

    Baxter, A.D. / Greenwood, S.W. | Emerald Group Publishing | 1958