Summary of a detailed engineering study conducted to evaluate the potential of composite engines when applied to the first stage of a two-stage manned advanced reusable launch vehicle. A total of 36 composite engines were evaluated for this mission/application. In all cases considered, composite engines were clearly shown to be superior when compared to an advanced liquid rocket engine. Payload in orbit results are presented for the more attractive composite engines. In addition, vehicle payload performance as a function of vehicle staging velocity is presented. Typical staging velocities are Mach 8 to 10.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Composite propulsion systems for an advanced reusable launch vehicle application


    Beteiligte:
    Bendot, J. G. (Autor:in)

    Kongress:

    International Symposium on Air Breathing Engines ; 1974 ; Sheffield


    Erscheinungsdatum :

    01.01.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    PROPULSION UNIT FOR REUSABLE LAUNCH VEHICLE

    CORABOEUF YOHANN / DUTHEIL JEAN-PHILIPPE | Europäisches Patentamt | 2016

    Freier Zugriff

    Propulsion unit for reusable launch vehicle

    CORABOEUF YOHANN / DUTHEIL JEAN-PHILIPPE | Europäisches Patentamt | 2016

    Freier Zugriff

    PROPULSION UNIT FOR REUSABLE LAUNCH VEHICLE

    KORABOEF JOKHANN / DYUTEL ZHAN-FILIPP | Europäisches Patentamt | 2018

    Freier Zugriff

    Propulsion unit for reusable launch vehicle

    CORABOEUF YOHANN / DUTHEIL JEAN-PHILIPPE | Europäisches Patentamt | 2018

    Freier Zugriff

    Reusable Launch Vehicle (RLV) Propulsion Technology

    Lee, J. E. / United States; National Aeronautics and Space Administration | British Library Conference Proceedings | 1996