Master Curve Method of Cumulative Damage for Prediction of Service Life

目的研究固体火箭推进剂药柱贮存使用寿命预测的理论与方法．方法采用非接触测试技术和热加速老化累积损伤法，实测得出药柱空穴率随老化时间变化的等温线，根据时温等效原理求得使用寿命预测粘弹性主曲线．结果与结论预测得出ＨＭＸＣＭＤＢ固体火箭推进剂药柱的使用寿命．由于该方法中药柱贮存失效的临界点是实测的，所以大大地提高了火箭推进剂药柱使用寿命预测的精度．

Aim To study the theory and method for the prediction of service life of solid rocket propellant grain. Methods With the aid of discontiguous diagnostic technology and method of accumulated damage using accelerated aging or heat air oven, the aging isotherms for void content versus aging time were determined. According to the principle of time temperature equivalence the viscoelastic master curve for the prediction of service life were obtained. Results and Conclusion The service life of HMX CMDB solid rocket propellant grain were obtained. Because the critical storage life is measured, the accuracy of predicting the service life of the grain has been increased greatly.