Evaporation of Plasticizer from NEPE Type Propellant

被引:0
|
作者
Yu. M. Milekhin
A. A. Koptelov
N. I. Shishov
I. A. Koptelov
A. A. Rogozina
机构
[1] Federal Center of Dual-Use Technologies “Soyuz,
[2] ”,undefined
来源
关键词
D O I
暂无
中图分类号
学科分类号
摘要
Using the method of dynamic thermogravimetry and differential scanning calorimetry in the heating rate range 0.46–10.0 deg–1 min–1, evaporation of the plasticizer from propellant samples of the NEPE type was investigated. The experiments were carried out in an open system in a flow of pure argon at atmospheric pressure. Nitroglycerin is the main mass fraction of the plasticizer. The activation energy E of the gross evaporation–diffusion process is determined by various methods. Heat of evaporation of the plasticizer ΔHv is estimated. It is shown that in the early stage of evaporation the values of E and ΔHv practically coincide. At a temperature of 298.15 K ΔHv = 89 ± 4 kJ mol–1, which is in satisfactory agreement with the literature data for heat of evaporation of pure nitroglycerin. With any way of preventing free removal of the plasticizer from the surface of the samples on the DSC thermograms successive exothermic peaks of the thermal decomposition of the plasticizer and the octogen are observed, which are not realized in the open system for the indicated heating rates at T < 190°C.
引用
收藏
页码:802 / 812
页数:10
相关论文
共 50 条
  • [21] Combustion process and aluminum agglomeration characteristics of NEPE propellant
    Tu C.
    Zhuang Y.
    Li Y.
    Zhou C.
    Cai W.
    Chen X.
    Li W.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (11): : 2791 - 2798
  • [22] Combustion peculiarity of condensed-products of NEPE propellant
    Zhao, Zhi-Bo
    Liu, Pei-Jin
    Zhang, Shao-Yue
    Gan, Xiao-Song
    Tuijin Jishu/Journal of Propulsion Technology, 2010, 31 (01): : 69 - 73
  • [23] Thermal decomposition of NEPE propellant with CL-20
    Xi'an Modern Chemistry Research Institute, Xi'an 710065, China
    Guti Houjian Jishu, 2008, 3 (251-254):
  • [24] Molecular Dynamics Simulation of the Pyrolysis and Oxidation of NEPE Propellant
    Wen, Zhengcheng
    Zhao, Xiang
    Li, Heping
    Huang, Xuefeng
    Wang, Fang
    Li, Wei
    Tang, Gen
    Feng, Muye
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2022, 47 (12)
  • [25] Qualitative analysis of migration components in the interface of NEPE propellant
    Huang, Zhi-Ping
    Liu, Juan-Ji
    Xu, Sheng-Liang
    Bai, Jie
    Ma, Xin-Gang
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (05): : 541 - 544
  • [26] Molecular simulation study of the stabilization process of NEPE propellant
    Ling-ze Kong
    Ke-hai Dong
    Ai-min Jiang
    Chuan-lu Yang
    Yan-hui Tang
    Yun-dong Xiao
    Defence Technology, 2023, 25 (07) : 220 - 230
  • [27] Experimental study on DDT of NEPE propellant at weak confinement
    Baozha Yu Chongji Bianjibu, 4 (312):
  • [28] Study on the Viscoelastic Damage Properties of NEPE Solid Propellant
    Hu, Qinwei
    Fang, Qin-Zhi
    Sha, Baolin
    Xu, Qiang
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2020, 45 (07) : 1076 - 1087
  • [29] The Characteristics of Static and Dynamic Mechanical Properties of NEPE propellant
    Gao, Yan-bin
    Chen, Xiong
    Xu, Jin-sheng
    Hu, Shao-qing
    PROCEEDINGS OF 2014 INTERNATIONAL CONFERENCE ON MECHANICS AND MECHANICAL ENGINEERING, 2014, 684 : 111 - 116
  • [30] Effect of additives on the mechanical property of NEPE propellant (I)
    Pang, A.
    Wu, J.
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2001, 24 (01): : 35 - 38