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:
    Meade, Brian (author) / Talley, Doug (author) / Mueller, Donn (author) / Tew, Dave (author) / Guidos, Mike (author) / Seymour, Dave (author)

    Conference:

    Aerospace Sciences Meeting and Exhibit ; 2001 ; Reno, NV, United States


    Publication date :

    2001-01-10


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English