Paper considers, analytically and experimentally, feasibility of rocket motor using detonation wave rotating in annular combustion chamber wherein propellants are introduced continuously through injectors and expelled through annular nozzle; experiments utilizing gaseous hydrogen and oxygen and gaseous methane and oxygen were conducted in annular rocket motor; single Chapman-Jouguet wave was realized successfully for first cycle but subsequent cycles of wave were not obtained; analyses indicated that such motor is feasible and therefore worth consideration.


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    Titel :

    Feasibility studies of rotating detonation wave rocket motor


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Nicholls, J.A. (Autor:in) / Cullen, R.E. (Autor:in) / Ragland, K.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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