The metallic wall of the combustion chamber of a combined rocket-ramjet engine is lined with solid ramjet fuel overlaid with rocket fuel. After the consumption of the rocket fuel in the boost portion of the flight the solid ramjet fuel burns and ablates protecing the metallic combustion chamber wall from high temperatures during the cruise of the missile flight. (Author)


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    Title :

    Combined Cycle Ramjet Engine


    Contributors:
    J. R. Smith (author)

    Publication date :

    1979


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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