An evaluation of reusable thrust chambers for the space shuttle orbit maneuvering engine was conducted. Tests were conducted using subscale injector hot-fire procedures for the injector configurations designed for a regenerative cooled engine. The effect of operating conditions and fuel temperature on combustion chamber performance was determined. Specific objectives of the evaluation were to examine the optimum like-doublet element geometry for operation at conditions consistent with a fuel regeneratively cooled engine (hot fuel, 200 to 250 F) and the sensitivity of the triplet injector element to hot fuels. (Author)


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    Titel :

    Space Shuttle Orbit Maneuvering Engine, Reusable Thrust Chamber Program. Task 6: Data Dump Hot Fuel Element Investigation


    Beteiligte:
    W. H. Nurick (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch