推进剂
阿累尼乌斯方程
加速老化
稳定器(航空)
动力学
化学动力学
反应速率
化学
分解
高能材料
热力学
阿伦尼乌斯图
材料科学
反应机理
过程(计算)
反应级数
化学分解
化学反应
反应速率常数
活化能
扫描电子显微镜
降级(电信)
质谱法
速率方程
作者
Jin Li,Tian Tian,Guan Zhang,Zongkuan Liu,Zhaolin Gu,Jiaxin Niu
标识
DOI:10.1002/prep.202100017
摘要
Abstract The prediction and determination of shelf‐life is an important step in the storage and use of ammunition. In this study, the aging reaction model and shelf‐life prediction model of SF‐3 double‐base propellant were studied. First, a theoretical aging reaction model of SF‐3 was developed based on scanning electron microscopy and energy‐dispersive X‐ray spectroscopy analysis and the aging reaction process. The aging reaction model was also experimentally validated. Then, based on the theoretical aging reaction model and the Arrhenius equation, the stabilizer depletion and mass loss kinetics models were developed. The aging reaction model showed a linear relationship between the stabilizer depletion rate x n and the aging time t , which indicated that the aging reaction is a zero‐order reaction. The rate‐limiting step of the SF‐3 aging reaction was the decomposition rate of nitrate ester compounds. The reaction kinetics model showed that the equation to predict the shelf‐life of SF‐3 was t [d]=1.44×10 −13 exp(11428.38/ T [K]). Additionally, the relationship between the mass loss rate x w and storage temperature T was x w [%]=53.93exp(−446.97/ T [K]) at the end of the shelf‐life of SF‐3. The results of this study provide a reference for predicting the aging process of other propellants that use nitrate ester compounds as the main energetic components. It also provides theoretical support for using the mass loss rate to predict the shelf‐life of SF‐3.
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