When pulsing rocket engines are tested under altitude conditions, data show that probability of large ignition overpressures generally decreases as temperature of rocket engine increases; this trend suggests that large ignition overpressures are related to accumulations of energy-rich substances on internal surfaces of engine; analytical and experimental investigation of this hypothesis and of means for insuring smooth ignition of pulsing rocket engines are presented; results show that large ignition overpressures can be avoided if engine walls are kept warm enough to prevent residual materials from accumulating in combustion chamber during duty cycles being fired.


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    Titel :

    Ignition transients in small hypergolic rockets


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Juran, W. (Autor:in) / Stechman, R.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Ignition transients in small hypergolic rockets.

    JURAN, W. / STECHMAN, R. C. | AIAA | 1968


    Ignition transients in small hypergolic rockets

    JURAN, W. / STECHMAN, R. | AIAA | 1967


    Ignition transients in small hypergolic rockets.

    Juran, W. / Stechman, R. C. | NTRS | 1968


    Starting Transients Of Hypergolic Bipropellant Rockets

    Bollinger, Loren E. / Lemmon, Jr. Alexis W. / Goldsmith, Martin | AIAA | 1960


    Investigation of Green Hypergolic Propellants for Hybrid Rockets

    Stober, Keith Javier / Thomas, Anna / Evans, Brian J. et al. | AIAA | 2016