This report presents the results of the test matrix development for design verification at the component level for the National Launch System (NLS) space transportation main engine (STME) thrust chamber assembly (TCA) components including the following: injector, combustion chamber, and nozzle. A systematic approach was used in the development of the minimum recommended TCA matrix resulting in a minimum number of hardware units and a minimum number of hot fire tests.


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    Titel :

    Design Verification Test Matrix Development for the STME Thrust Chamber Assembly


    Beteiligte:
    C. E. Dexter (Autor:in) / S. K. Elam (Autor:in) / D. L. Sparks (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    40 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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