Effect of nitramine on energy and burning rate of low burning rate HTPB propellant

被引：0
|
作者：
Lu, G. [1 ]
机构：
[1] The 42nd Inst. of the Fourth Acad., CASC, Xiangfan 441003, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2001年 / 24卷 / 02期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
An application investigation of the nitramine (RDX,HMX) to the low burning rate HTPB propellants was carried out in the view of energetic property and combustion performance. The results show that the partial substitution of nitramine for ammonium perchlorate can raise theoretical specific impulse and reduce pressure exponent of propellants greatly, while the effect on burning rate is very minor.
引用
收藏
页码：45 / 47
相关论文
共 50 条
  • [1] Study on burning-rate control of low burning-rate HTPB propellant
    Cui, Ruixi
    Tuijin Jishu/Journal of Propulsion Technology, 1999, 20 (02): : 77 - 82
  • [2] Allowances control of the burning rate of medium burning-rate HTPB propellant
    Guti Houjian Jishu, 2 (35):
  • [3] Study on the formulation of low burning rate HTPB propellant with RDX
    Cao, Wen-Zhong
    Wang, Zhong-Wei
    Jiao, Shao-Qiu
    Zhang, Wei-Hua
    Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2009, 32 (05): : 54 - 57
  • [4] Process Performance of Low Aluminum and Low Burning Rate HTPB Propellant
    Zhang N.
    Liang B.
    Liu J.-X.
    Gao W.-P.
    Xin Y.-P.
    Liu C.-Y.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (03):
  • [5] Effect of Aluminum Morphology on Burning Rate Characteristics of HTPB Propellant
    Zhu, Li-Xun
    Liang, Bei
    Liu, Jin-Xiang
    Zhang, Wei-Hai
    Yan, Wu-Qi
    Liao, Xin
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2017, 25 (10): : 799 - 803
  • [6] Effect of spherical aluminum on combustion behavior of low burning-rate HTPB propellant
    Jiao, Ji-ge
    Zhou, Ke
    Zhang, Wei
    Hanneng Cailiao/Energetic Materials, 2000, 8 (02): : 72 - 74
  • [7] Regulation of burning rate and analysis of cost for HTPB propellant
    Guti Houjian Jishu, 2 (36-40):
  • [8] Erosive burning model identification of a propellant with low burning rate
    Yang, Xuan
    Zhao, Dong-Ming
    Yu, Zhen-Yong
    Yuhang Xuebao/Journal of Astronautics, 2008, 29 (06): : 1932 - 1935
  • [9] Study on Decreasing the Mechanical Sensitivity of HTPB Propellant with High Burning Rate
    Pang A.-M.
    Liu X.
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2019, 27 (11): : 961 - 966
  • [10] Effect of antioxidant on properties of high burning rate HTPB-IPDI propellant (II)
    Lu, Guo-lin
    Liu, Xue
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2000, 23 (03): : 34 - 36
12345