The patent application relates to the design of a ramjet engine whereby air injection ports and fuel injection systems are arranged in a manner to enhance flame stability.


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    Titel :

    Integral Rocket/Ramjet Propulsion System with Axial Admission Ports


    Beteiligte:
    E. T. Curran (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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