By employing uniaxial viscoelastic propellant data, it is demonstrated that normally neglected thermal gradients in propellant can significantly affect the results of a stress analysis in solid propellant rocket grains. The problems related to the direct measurement of stresses in solid propellant are identified and reviewed, and an appropriate stress transducer is proposed. (Author)


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    Titel :

    Temperature Gradients and Stress Measurement in Solid Propellants


    Beteiligte:
    A. San Miguel (Autor:in) / E. N. Duran (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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