The configuration of reusable solid propellant motors for the space shuttle vehicle is delineated and traces their design evolution. Also presented are the summary results of the first two of the three qualification motor firings designated QM-1 and QM-2.


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    Title :

    Space Shuttle Solid Rocket Motor (SRM) development and qualification


    Contributors:


    Publication date :

    1980-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English