Problems which the solid propellant rocket engineer will encounter in designing for long-term storage in a radiation environment are discussed. A summary of present knowledge of the radiation environment is given. Mechanisms of radiation degradation and its effects on tensile properties of propellant binders are discussed qualitatively. Data from a program of irradiation of several propellants is presented. Properties of two of the propellants were changed significantly by doses of the order of 4 x 10(exp 6) rads.


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    Title :

    Effects of Ionizing Radiation on Solid Rocket Motor Components


    Contributors:

    Publication date :

    1961-12-21


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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