A propulsion system analysis of the dual fuel, dual throat engine for launch vehicle applications was conducted. Basic dual throat engine characterization data were obtained to allow vehicle optimization studies to be conducted. A preliminary baseline engine system was defined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren




    Heat Flux In A Dual-Throat Rocket Engine

    Ewen, R. L. / Obrien, C. J. | NTRS | 1989



    Preliminary Analysis and Design Enhancements of a Dual-Throat FTV Nozzle Concept

    Bellandi, E. / Slippey, A. / American Institute of Aeronautics and Asronautics | British Library Conference Proceedings | 2009