高氯酸铵
热分解
催化作用
推进剂
分解
氮气
燃烧
化学
金属有机骨架
活化能
无机化学
复合数
材料科学
化学工程
物理化学
有机化学
复合材料
工程类
吸附
作者
Wen-chuan Cheng,Jiamin Chen,You‐Nian Liu,Huisheng Huang,Jian Guo Zhang,Tonglai Zhang,Zhimin Li
标识
DOI:10.1016/j.enmf.2023.03.001
摘要
With the development of aerospace science and technology, requirements for propellants are increasingly high. The thermal decomposition behavior of ammonium perchlorate (AP) directly influences the combustion performance of composite solid propellants. Catalysts play an important role in improving the thermal decomposition behavior of AP. In this study, three novel metal-organic frameworks (MOFs) were prepared using a straightforward method, namely Co[N(CN)2]2 (1; nitrogen content: 43.5%), Cu[N(CN)2]2 (2; nitrogen content: 43.0%), and Pb[N(CN)2]2 (3; nitrogen content: 24.8%). Their crystal structures were characterized and analyzed through single-crystal X-ray diffraction, forming interesting three-dimensional architectures. Moreover, derived composite catalysts under air (4, 6, and 8) or nitrogen (5, 7, and 9) atmosphere were generated by heating MOFs 1, 2, and 3–500 °C at a heating rate of 5 °C·min−1. The derived catalyst 4 exhibited the best performance. It reduced the decomposition peak temperature of AP by 81.9 °C, increased the heat release from 785 kJ·g−1 to 1232 kJ·g−1, and decreased the apparent activation energy (Ea) of AP from 223 kJ·mol−1 to 145 kJ·mol−1.
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