Uncooled rocket engine was investigated over chamber pressure from 45 to 300 psia and oxidant-fuel ratio from 2 to 7; combustion dead times were calculated from chamber-pressure frequency measurements; dead time decreased with increased chamber pressure at constant oxidant-fuel ratio or liquid-oxygen injection velocity; close agreement obtained between measured dead times and those calculated from frequency measurements.


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    Titel :

    Relations of combustion dead time to engine variables for 20,000-pound-thrust gaseous-hydrogen-liquid-oxygen rocket engine


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Drain, D.I. (Autor:in) / Schum, H.J. (Autor:in) / Wasserbauer, C.A. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :