Abstract The ejector ramjet, one kind of rocket-based combined cycle propulsion, has received increasing attention lately as a potential solution for reusable air-breathing space transportation systems. This paper discusses a system study of an ejector ramjet and presents a method for the optimization of the trajectory and engine parameters. Due to the potentially large number of input parameters and their sensitivities on the overall system performance, a hybrid genetic algorithm was chosen for the optimization.


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    Titel :

    System Analysis and Trajectory Optimization of an Ejector-Ramjet Powered Reusable Launch Vehicle


    Beteiligte:
    Shepperd, R. (Autor:in) / Lentsch, A. (Autor:in) / Maita, M. (Autor:in) / Mori, T. (Autor:in)


    Erscheinungsdatum :

    01.01.2000


    Format / Umfang :

    5 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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