The catalytic thermal decomposition of ammonium perchlorate on CuMxOy (M = Fe, Ni, Co and Zn) catalysts and their applications in solid propellant

被引:4
作者
Hu, Yinghui [1 ,2 ]
Wang, Xuwen [1 ]
Hao, Jingwei [1 ]
Jiang, Shouhang [1 ]
Zhang, Jian [1 ]
Yang, Yulin [1 ]
Lin, Kaifeng [1 ]
Zheng, Jian [3 ]
Shuai, Yong [2 ]
机构
[1] Harbin Inst Technol, Sch Chem & Chem Engn, MIIT Key Lab Crit Mat Technol New Energy Convers &, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China
[3] China Aerosp Sci & Technol Corp, 16 Fucheng Rd, Beijing 100048, Peoples R China
关键词
Bimetal oxide catalyst; Ammonium perchlorate; Thermal decomposition; Catalytic mechanism; Burning rate; COMBUSTION CHARACTERISTICS; COMPOSITE PROPELLANTS; RGO/MFE2O4; M; PERFORMANCE; NANOPARTICLES; NANOCOMPOSITE; FABRICATION; IGNITION; BEHAVIOR; CO3O4;
D O I
10.1007/s10973-023-12156-7
中图分类号
O414.1 [热力学];
学科分类号
摘要
The excellent thermal decomposition efficiency of ammonium perchlorate (AP) is of great importance for obtaining propellant with fast specific impulse. In this study, four CuMxOy catalysts, including M = Fe, Ni, Co, and Zn, were synthesized and then used for catalyzing AP decomposition and hydroxyl-terminated polybutadiene (HTPB)-based solid propellant combustion. The existed synergistic effect in CuMxOy catalysts improved the catalytic activity and the most active CuZnO catalyst decreased the AP high-temperature decomposition temperature (HTD) from 412.5 to 289.4 ?. Kinetic studies indicated that CuMxOy catalysts inhibited the conversion of N2O to a fully oxidized product and decreased the activation energy (E-a) in HTD to concentrate AP decomposition to significantly decrease the heat loss, thereby increasing their decomposition efficiency. When applying the CuMxOy catalysts in the HTPB (hydroxyl-terminated polybutadiene)-based solid propellant, a faster burning rate and stronger optical emission spectrum were obtained. The CuMxOy catalyst is a potential additive for the preparation of outstanding combustion solid propellants.
引用
收藏
页码:6013 / 6026
页数:14
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