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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    Titel :

    Advanced Thrust Chamber for Space Maneuvering Propulsion


    Beteiligte:
    H. G. Diem (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    88 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch