A study has been conducted which deals with the feasibility of utilizing exclusively the detonative mode of combustion in a rocket motor rather than the deflagrative mode used in conventional, chemical rocket motors. The configuration adopted consists of an annular combustion chamber wherein detonation waves completely fill the chamber cross-section and propagate steadily in the same circumferential direction. This configuration leads to the descriptive term Rotating Detonation Wave Engine (RDWE). (Author)


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    Titel :

    The Feasibility of a Rotating Detonation Wave Rocket Motor


    Beteiligte:
    J. A. Nicholls (Autor:in) / R. E. Cullen (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    220 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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