This paper presents a performance model rocket engine design that takes advantage of pulse detonation to generate thrust. The contents include: 1) Introduction to the Pulse Detonation Rocket Engine (PDRE); 2) PDRE modeling issues and options; 3) Discussion of the PDRE Performance Workshop held at Marshall Space Flight Center; and 4) Identify needs involving an open performance model for Pulse Detonation Rocket Engines. This paper is in viewgraph form.


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    Titel :

    Future Modeling Needs in Pulse Detonation Rocket Engine Design


    Beteiligte:
    B. Meade (Autor:in) / D. Talley (Autor:in) / D. Mueller (Autor:in) / D. Tew (Autor:in) / M. Guidos (Autor:in)

    Erscheinungsdatum :

    2001


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch