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THE CREEP-DAMAGE MODELING CORRELATED TO TEMPERATURE FOR COMPOSITE SOLID PROPELLANT |
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| Authors: | Shen Huairong |
| Abstract: | The creep-damage modeling correlated to temperature has been described fora kind of composite solid propellant (CSP) in this paper. The material parameters of themodeling were determined by creep experiments of uniaxial and biaxial loading. The modeling is useful for analysis of solid rocket motor and for prediction of service life of the CSP. |
| Keywords: | composite solid propellant creep damage temperature |
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