Researches on thermal decomposition kinetics of composite modified double-base propellants

Zhan Tang*, Yan Ren, Li Yang, Tonglai Zhang, Xiaojing Qiao, Jianguo Zhang, Zunning Zhou, Fengqi Zhao, Yongzhan Dang, Siyu Xu, Jianhua Yi

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

The thermal decomposition kinetics of composite modified double-base (CMDB) propellants with a series of contents of hexogeon (RDX) was investigated by using parameters of Teo, Ti, Tp, Tf, Tb, Ta, E, lg A and ΔH, which were obtained from using a CDR-4P differential scanning calorimeter (DSC) and Perkin-Elmer Pyris 1 thermogravimetric analyzer (TG) analyses with heating rates of 5, 10, 15 and 20 K/min. Reliable activation energy was calculated using Flynn-Wall-Ozawa method before analyzing the thermal decomposition mechanism. TG-DTG curves were treated with Malek method in order to obtain the reaction mechanisms. The obtained results show that the thermal decomposition mechanisms with the conversion from 0.2 to 0.4 was f(α) 1/2α, and with the conversion from 0.5 to 0.7 was f(α)=(1/4)(1-α)[-ln(1-α)]-3.

源语言英语
页(从-至)411-414
页数4
期刊Chinese Journal of Chemistry
29
3
DOI
出版状态已出版 - 3月 2011

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