The patent relates to a method whereby a plurality of perforated tubes are placed longitudinally between the insulator layer and silicone rubber layer of a stress relieving rocket motor liner to insure proper pressure distribution within the motor during burn.


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    Title :

    Rocket Motor Apparatus


    Contributors:

    Publication date :

    1974


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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