Model illustrating application of techniques employed is solid-propellant grain made of urethane rubber and case-bonded to relatively rigid transparent motor case, through which light beam can pass; transition from model to prototype stress is direct, since model material is similar to binder material in existing propellants; shrinkage stresses are induced by uniform temperature change simulating conditions imposed on propellants in storage; loaded propellant model is examined with polarized laser light source; resulting scattered fringe patterns and principal stress axes are used to evaluate stress distribution. (28528)


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    Titel :

    Scattered light photoelastic thermal stress analysis of solid-propellant rocket motor


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Braswell, D.W. (Autor:in) / Ranson, W.F. (Autor:in) / Swinson, W.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Scattered light photoelastic thermal stress analysis of a solid-propellant rocket motor.

    BRASWELL, D. W. / RANSON, W. F. / SWINSON, W. F. | AIAA | 1968




    Solid Propellant Rocket Motor Thermal Analysis

    Heatherly, E. R. / Gonzalez, J. I. | SAE Technical Papers | 1962


    Solid propellant rocket motor thermal analysis

    Heatherly, E.R. / Gonzalez, J.K. | Engineering Index Backfile | 1962