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
  • [41] Mechanical properties of NEPE propellant containing two coated ε-HNIW
    Meng, Zheng
    Ou, Yu-Xiang
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2008, 16 (01): : 60 - 62
  • [42] Study on the constitutive model of NEPE propellant based on indentation creep
    Liu, Zai
    Qiang, Hongfu
    Hui, Weiwei
    Zhang, Yurou
    Cao, Peng
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2023, 48 (12)
  • [43] Quantitative method for monitoring stabilizers content of NEPE propellant by FTIR
    Wan, Qian
    Sui, Xin
    Wang, Ning-Fei
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2013, 36 (02): : 274 - 277
  • [44] Theoretical Calculation and Numerical Simulation of Thermal Safety on NEPE Propellant
    Qin P.-W.
    Wang M.-L.
    Lu R.-H.
    Guo C.-L.
    Huang C.-L.
    Li Y.
    Zhao X.-B.
    Peng S.
    Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2019, 42 (06): : 602 - 607and613
  • [45] A promising azido nitrate ester plasticizer for propellant
    Yang, Junqing
    Gong, Xuedong
    Wang, Guixiang
    COMPUTATIONAL MATERIALS SCIENCE, 2015, 110 : 71 - 76
  • [46] Research on the time–temperature–damage superposition principle of NEPE propellant
    Long Han
    Xiong Chen
    Jin-sheng Xu
    Chang-sheng Zhou
    Jia-quan Yu
    Mechanics of Time-Dependent Materials, 2015, 19 : 581 - 599
  • [47] Theoretical study on the pyrolysis mechanism of key components of NEPE propellant
    Wen, Zhengcheng
    Wu, Yiyi
    Li, Heping
    Huang, Xuefeng
    Wang, Fang
    Li, Wei
    Tang, Gen
    Feng, Muye
    SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2023, 84 (05) : 60 - 71
  • [48] Molecular Simulation Study on the Aging Mechanism of NEPE Propellant Matrix
    Kong, Lingze
    Dong, Kehai
    Tang, Yanhui
    Yang, Chuanlu
    Xiao, Yundong
    MOLECULES, 2023, 28 (04):
  • [49] Molecular dynamics study on the effect of pressure on the combustion of NEPE propellant
    Wen, Zhengcheng
    Chang, Mingrui
    Li, Heping
    COMBUSTION THEORY AND MODELLING, 2025,
  • [50] Experimental Investigation on Laser Ignition and Combustion Characteristics of NEPE Propellant
    Li, Lian-Bo
    Chen, Xiong
    Zhou, Chang-Sheng
    Zhu, Min
    Musa, Omer
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2017, 42 (09) : 1095 - 1103