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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aft Inlet Ramjet Powered Missile


    Contributors:

    Publication date :

    1973


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    AFT Inlet Ramjet Powered Missile

    D. B. Wilkinson | NTIS | 1973


    Ramjet Powered Missile Design Using I Genetic Algorithm

    Hartfield, R. J. / Jenkins, R. M. / Burkhalter, J. E. et al. | British Library Conference Proceedings | 2004


    Ramjet Powered Missile Design Using a Genetic Algorithm

    Hartfield, Roy / Jenkins, Rhonald / Burkhalter, John | AIAA | 2004



    Genetic Algorithm Design Results for a Ramjet Powered Missile

    Hartfield, Roy / Jenkins, Rhonald / Burkhalter, John | AIAA | 2004