An investigation was performed on an improved Space Shuttle Main Engine (SSME) hot gas manifold (HGM) design using a full scale HGM model in cold-flow, air-blowdown tests. The new HGM design replaces the current three transfer ducts with two enlarged elliptical transfer ducts, faired duct inlets, and enlarged fuel bowl. Extensive experimental results have been obtained to verify previous results showing that the two-duct design improved the HGM internal flow path by eliminating separated flow regions, reducing high local velocities, and providing more uniform flow.


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    Titel :

    Experimental aerodynamic evaluation of the SSME two-duct, hot gas manifold


    Beteiligte:
    Kim, B. Y. (Autor:in) / Cuan, W. M. (Autor:in) / Oconnor, G. M. (Autor:in) / Richards, D. R. (Autor:in)


    Erscheinungsdatum :

    01.08.1986


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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