Catalysis combustion property and mechanism of PDADN-RDX-CMDB propellant

被引:0
|
作者
Li, S.F. [1 ]
Wang, J. [1 ]
Zhao, F.Q. [1 ]
Wang, Y. [1 ]
Xu, Y. [1 ]
Li, S.W. [1 ]
机构
[1] Dep. of Chem. Phys., Univ. of Sci. and Technol., Hefei 230026, China
来源
关键词
Catalysis; -; Catalysts; Combustion;
D O I
暂无
中图分类号
学科分类号
摘要
In order to study effects of several kinds of composite catalysts on the combustion behavior of PDADN-RDX-CMDB propellant, different means such as thermogravimetric loss, microthermo couple, burning-rate experiment and SEM of quenched sample surface were adopted. The results show that two kinds of composite catalysts, which are ΦPb-βCu-Cb and βPbCu-CB, can obviously improve the combustion behavior of PDADN-RDX-CMDB propellant, combustion pressure exponent are decreased and burning-rate are increased. The 'bubble-condensation reaction' theory are proposed to explain 'super rate combustion' phenomenon of PDADN-RDX-CMDB with composite catalysts propellant.
引用
收藏
页码:165 / 170
相关论文
共 50 条
  • [31] Modeling of RDX/GAP/BTTN pseudo-propellant combustion
    Yoon, JK
    Thakre, P
    Yang, V
    [J]. COMBUSTION AND FLAME, 2006, 145 (1-2) : 300 - 315
  • [32] Study on combustion rate prediction model of CMDB propellant with fine grained AP
    Feng, Feng
    Chen, Jun
    Song, Hong-Chang
    Zheng, Ya
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2010, 31 (03): : 356 - 360
  • [33] Effects of nano-HMX on the properties of RDX-CMDB propellant:Higher energy and lower sensitivity
    Han GAO
    Xiao-ting HOU
    Xiang KE
    Jie LIU
    Gazi HAO
    Lei XIAO
    Teng CHEN
    Ying-ying ZUO
    Wei JIANG
    [J]. Defence Technology, 2017, 13 (05) : 323 - 326
  • [34] Relationships between combustion and condensed phase thermal decomposition of HMX - CMDB propellant
    Jia, Huiping
    Bai, Mulan
    [J]. Proceedings of the International Pyrotechnics Seminar, 1991, 1
  • [35] Effect of Al content and particle size on the combustion of HMX-CMDB propellant
    Xiao, Li-Qun
    Fan, Xue-Zhong
    Li, Ji-Zhen
    Qin, Zhao
    Fu, Xiao-Long
    Pang, Wei-Qiang
    Wang, Ying
    [J]. COMBUSTION AND FLAME, 2020, 214 (214) : 80 - 89
  • [36] Effects of nano-HMX on the properties of RDX-CMDB propellant: Higher energy and lower sensitivity
    Gao Han
    Hou Xiao-ting
    Ke Xiang
    Liu Jie
    Hao Gazi
    Xiao Lei
    Chen Teng
    Zuo Ying-ying
    Jiang Wei
    [J]. DEFENCE TECHNOLOGY, 2017, 13 (05): : 323 - 326
  • [37] The effect of strain rate on compressive behavior and failure mechanism of CMDB propellant
    Heng-ning Zhang
    Hai Chang
    Xiao-jiang Li
    Xiong-gang Wu
    Qi-wen He
    [J]. Defence Technology, 2022, (03) : 467 - 475
  • [38] The effect of strain rate on compressive behavior and failure mechanism of CMDB propellant
    Heng-ning Zhang
    Hai Chang
    Xiao-jiang Li
    Xiong-gang Wu
    Qi-wen He
    [J]. Defence Technology, 2022, 18 (03) : 467 - 475
  • [39] The effect of strain rate on compressive behavior and failure mechanism of CMDB propellant
    Zhang, Heng-ning
    Chang, Hai
    Li, Xiao-jiang
    Wu, Xiong-gang
    He, Qi-wen
    [J]. DEFENCE TECHNOLOGY, 2022, 18 (03) : 467 - 475
  • [40] Effect of Carbon Nanotubes on the Catalysis of Propellant Combustion
    A. P. Denisyuk
    Y. M. Milekhin
    L. A. Demidova
    V. A. Sizov
    [J]. Doklady Chemistry, 2018, 483 : 301 - 303