Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant. The primary purpose is to prevent the case from reaching temperatures that endanger its structural integrity. Secondary functions of the insulation are listed and guidelines for avoiding critical problems in the development of internal insulation for rocket motors are presented.


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    Title :

    Solid rocket motor internal insulation


    Contributors:

    Publication date :

    1976-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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