An effective capability for testing the Space Shuttle Main Engine is described. The test complex utilizes a number of sophisticated test stands, test support facilities, and control centers to conduct development testing and flight acceptance testing at both nominal and off-nominal conditions.


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    Title :

    SSME testing technology at the John C. Stennis Space Center


    Contributors:
    Kynard, Mike (author) / Dill, Glenn (author)

    Publication date :

    1991-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English