For winged, horizontal take off and landing vehicule, the propulsion system appears as one of the key technologies. Based on the progresses in advanced technologies like cryogenic propulsion, high temperature materials, this paper will present progress on current concept studies of airbreathing/rocket combined engines with some consideratons on questions raised by the vehicule / engine system integration (air inlet / engine performances / aircraft trajectory and thrust requirements).


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    Title :

    Airbreathing Combined Engines for Space Transportation Systems


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Vehicle Conference ; 1988



    Publication date :

    1988-03-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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