The patent application concerns 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 incorporates a liquid or solid 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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    Title :

    Reverse Flow AFT Inlet Ramjet System


    Contributors:

    Publication date :

    1974


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Reverse Flow Aft Inlet Ramjet System

    E. T. Curran | NTIS | 1975


    Reverse Flow Aft Inlet Ramjet System

    E. T. Curran | NTIS | 1975


    Reverse Flow AFT Inlet Ramjet System

    E. T. Curran | NTIS | 1974



    Investigation of Two-Mode Ramjet/Scramjet Inlet

    Falempin, F. / Montazel, X. / Goldfeld, M. et al. | British Library Conference Proceedings | 1999