The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)


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    Titel :

    Parametric Study of Rocket Instability


    Beteiligte:
    J. R. Osborn (Autor:in) / D. W. Netzer (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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