Since most of the HTPB propellants possess similar aging mechanism, this model can be used to predict storage life of all HTPB propellants.
考虑到大部分HTPB推进剂的老化机理相似，所以该模型具有一定普遍性，适用于HTPB推进剂贮存期的预估。
In this paper, the effects of the storage temperature on the ageing characteristics of HTPB propellants have been studied.
本文研究了贮存温度对丁羟推进剂老化性能的影响。
The relationships between damage energies of HTPB propellants and storage ageing time were investigated by uniaxial repeated tensile test.
由单轴反复拉伸试验分别研究了含键合型防老添加剂和防老剂h的HTPB推进剂破坏能与贮存老化时间的关系。
Based on the ageing experimental results, the ageing dynamic equation of HTPB propellant is obtained. A calculation and reliability analysis for propellant storage life are also presented.
在分析老化实验数据的基础上，建立了丁羟推进剂老化的动力学方程，以此为基础预估了推进剂的贮存寿命，分析了贮存寿命的可靠性。
Based on the ageing experimental results, the ageing dynamic equation of HTPB propellant is obtained. A calculation and reliability analysis for propellant storage life are also presented.
在分析老化实验数据的基础上，建立了丁羟推进剂老化的动力学方程，以此为基础预估了推进剂的贮存寿命，分析了贮存寿命的可靠性。
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