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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    Title :

    Future Modeling Needs in Pulse Detonation Rocket Engine Design


    Contributors:
    B. Meade (author) / D. Talley (author) / D. Mueller (author) / D. Tew (author) / M. Guidos (author)

    Publication date :

    2001


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English