The structural properties of solid propellant rocket grains were studied to determine the propellant resistance to stresses. Grain geometry, thermal properties, mechanical properties, and failure modes are discussed along with design criteria and recommended practices.


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    Title :

    Solid Propellant Grain Structural Integrity Analysis


    Publication date :

    1973-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :