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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    Titel :

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


    Beteiligte:
    S. A. Mullin (Autor:in) / P. A. Cox (Autor:in) / C. E. Anderson (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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