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 considerations on questions raised by the vehicule / engine system integration (air inlet / engine performances / aircraft trajectory and thrust requirements).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Airbreathing combined engines for space transportation systems


    Additional title:

    Kombinierte Antriebe mit Luftansaugung fuer Raumtransporter


    Contributors:

    Published in:

    SAE-Papers ; Apr ; 1-7


    Publication date :

    1988


    Size :

    7 Seiten, 14 Bilder


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Airbreathing Combined Engines for Space Transportation Systems

    Pouliquen, Marcel / Doublier, Michel | SAE Technical Papers | 1988


    Airbreathing engines for space shuttle

    Glassman, A. J. / Stewart, W. L. / Nosek, S. M. | NTRS | 1972


    Airbreathing Engines for Space Shuttle

    Glassman, Arthur J. / Nosek, Stanley M. / Stewart, Warner L. | SAE Technical Papers | 1972



    AIAA-2005-1204 OPTIMAL DESIGN FOR FUTURE SPACE TRANSPORTATION SYSTEMS USING AIRBREATHING ENGINES

    Suzuki, H. / Hirotani, T. / Kobayashi, H. et al. | British Library Conference Proceedings | 2005