The patent application relates to a solid fuel ramjet powered missile having the air inlets positioned adjacent the aft end of the fuel grain. A channel is provided adjacent the fuel grain to provide primary air into the forward end of the fuel grain with the secondary air being supplied directly to the secondary combustor. A valve is provided in the primary air flow channel to control the air flow into the fuel grain.


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    Titel :

    Aft Inlet Ramjet Powered Missile


    Beteiligte:

    Erscheinungsdatum :

    1973


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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