The patent application 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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    Titel :

    Ramjet with Integrated Rocket Boost Motor


    Beteiligte:
    J. H. Leingang (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ramjet with Integrated Rocket Boost Motor

    J. L. 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