The design of supersonic turbines for the Ariane 5 rocket motor is discussed. From the specification an optimization study was carried out. Influence factors led to requirements on the turbines where functions combining turbine weight, performance, development cost, production cost, and program risk were optimized. The full scale turbine produces a specific torque 7% lower than the subscale turbine. The performance is shown to be lower for both the stator and the rotor. Deviations which may explain the reduced performance are detailed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Design and Test Performance of Supersonic Turbines for the Vulcain Rocket Engine


    Beteiligte:
    H. A. Jergeus (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    VULCAIN X: Hydrogen/Oxygen Reusable Liquid Rocket Engine Demonstration

    Kachler, Thierry / Beaurain, Andre | AIAA | 2005


    Vulcain engine dynamic analysis

    ALLIOT, P. / DESNOT, F. / GAZAVE, R. | AIAA | 1990



    Air test flow analysis of the hydrogen pump of vulcain rocket engine

    Bario, F. / Barral, L. / Bois, G. | Tema Archiv | 1991