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).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Airbreathing combined engines for space transportation systems


    Weitere Titelangaben:

    Kombinierte Antriebe mit Luftansaugung fuer Raumtransporter


    Beteiligte:
    Doublier, M. (Autor:in) / Pouliquen, M. (Autor:in)

    Erschienen in:

    SAE-Papers ; Apr ; 1-7


    Erscheinungsdatum :

    1988


    Format / Umfang :

    7 Seiten, 14 Bilder


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Airbreathing Combined Engines for Space Transportation Systems

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


    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


    Development Activities on Airbreathing Combined Cycle Engines

    McArthur, J. Craig / Lyles, Garry | NTRS | 2000