Hardware design, fabrication and hot-firing test results for toroidal thrust chamber segments are discussed. Solid-wall segment testing has been conducted to evaluate injector and thrust chamber contour designs with respect to performance and heat transfer. Fabrication status of tube-wall throat inserts, tube wall segments, and structural test segments are presented. Hot firing test results for a tube wall throat insert are discussed. (Author)


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    Title :

    Advanced Thrust Chamber for Space Maneuvering Propulsion


    Contributors:
    H. G. Diem (author)

    Publication date :

    1967


    Size :

    88 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English