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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    Title :

    Integral Rocket/Ramjet Propulsion System with Axial Admission Ports


    Contributors:

    Publication date :

    1974


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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