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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    Titel :

    Combined Cycle Ramjet Engine


    Beteiligte:
    J. R. Smith (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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