A linear elastic finite element model of the Shrike missile was developed and run in a series of parametric studies to determine the effect of a cookoff-induced gas bubble upon the missile case and propellant. A series of case-to-liner interface. The model identified the critical gas bubble pressures to rupture the case or propellant, and evaluated the peel tests for their worthiness in the cookoff situation.


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    Title :

    Nondestructive Evaluation of Rocket Motors; Finite Element Analysis of Solid Propellant Failure


    Contributors:
    S. A. Mullin (author) / P. A. Cox (author) / C. E. Anderson (author)

    Publication date :

    1986


    Size :

    100 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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