The patent relates to a combined rocket/ramjet for propelling a missile including a missile payload module and an integral rocket/ramjet engine system strapped on the missile payload module. It includes a liquid fuel rocket engine and a ramjet engine having a combustion chamber common with the rocket engine, an exhaust nozzle, and multiple aft-mounted air inlets movable between a retracted position during rocket boost flight and an extended, pop-out position to receive and direct ram air in a reverse flow direction into the combustion chamber during ramjet flight.


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    Titel :

    Reverse Flow Aft Inlet Ramjet System


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

    Erscheinungsdatum :

    1975


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Reverse Flow AFT Inlet Ramjet System

    E. T. Curran | NTIS | 1974


    Reverse Flow Aft Inlet Ramjet System

    E. T. Curran | NTIS | 1975


    Reverse Flow AFT Inlet Ramjet System

    E. T. Curran | NTIS | 1974



    Conceptual study of a turbojet/ramjet inlet

    Weidner, John P. | TIBKAT | 1979