The propulsion system for the lower stage of a two-stage-to-orbit (TSTO) transport system is presented with its major components: mixed compression air intake, two-spool-low-bypass turbo engine and single expansion ramp nozzle. Intake and nozzle have been analysed by Navier-Stokes-calculations. Based on performance analysis a real time simulation program is presented, which has been integrated into a flight simulator. At hypersonic speeds the effects of the propulsion system on flight-mechanical behaviour is substantial, especially at engine failures. In a realistic flight-mechanical analysis of hypersonic aircraft the steady state and dynamic propulsion system performance has to be considered not only with axial thrust and drag components, but also with its significant lift and resulting pitching moments and stabilising effects on the aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Propulsion/aircraft integration and dynamic performance of hypersonic TSTO-vehicles


    Weitere Titelangaben:

    Antrieb/Luftfahrzeug-Integration und dynamische Leistung von zweistufigen Hyperschall-Raumtransportsystemen


    Beteiligte:
    Hollmeier, S. (Autor:in) / Esch, T. (Autor:in) / Herrmann, O. (Autor:in) / Rick, H. (Autor:in)


    Erscheinungsdatum :

    1995


    Format / Umfang :

    16 Seiten, 17 Bilder, 19 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Propulsion/Aircraft Integration and Dynamic Performance of Hypersonic TSTO Vehicles

    Esh, T. / Hollmeier, S. / Hermann, O. et al. | British Library Conference Proceedings | 1995


    Turboramjet propulsion for hypersonic booster-aircraft of TSTO aerospace system

    Lanshin, A. / Dulepov, N. / Zakharov, N. et al. | AIAA | 1996


    Turboramjet Propulsion for Hypersonic Booster-Aircraft of TSTO Aerospace System

    Dembo, N. / Lanshin, A. / Dulepov, N. et al. | British Library Conference Proceedings | 1996


    TSTO Reusable Launch Vehicles Using Airbreathing Propulsion

    Hank, Joseph / Franke, Milton / Eklund, Dean | AIAA | 2006


    TSTO Reusable Launch Vehicles Using Airbreathing Propulsion

    Hank, J. / Franke, M. / Eklund, D. et al. | British Library Conference Proceedings | 2006