Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant

被引:0
|
作者
Ling-ke Zhang [1 ]
Xiang-yang Zheng [1 ]
机构
[1] School of Energy and Power Engineering, Nanjing University of Science & Technology
关键词
Base bleed technology; AP/HTPB composite propellant; Natural ageing; Decomposition kinetics; DSC experiment;
D O I
暂无
中图分类号
TQ560.1 [基础理论]; TJ410 [一般性问题];
学科分类号
0817 ; 082603 ;
摘要
The kinetics of the thermal decomposition for a naturally ageing ammonium perchlorate(AP) and hydroxyl-terminated-polybutadiene(HTPB) base bleed composite propellant were investigated using a differential scanning calorimetry(DSC). The naturally ageing AP/HTPB base bleed propellant samples have been stored in a sealed plastic bag at room temperature(5-25 ℃) for more than 20 years. The experimental DSC results were obtained by placing samples(each about 1.5 mg) in a sealed pan under non-isothermal condition under different heating rates, 5.0, 10.0, 15.0, 20.0 and 30.0 ℃·min;. The activation energy and pre-exponential factor were estimated based on the relationship between the exothermic peak temperature and the heating rate by Ozawa and Kissinger methods, respectively. The decomposition kinetic parameters is lower the values under laboratorial aging condition.
引用
收藏
页码:422 / 425
页数:4
相关论文
共 50 条
  • [1] Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant
    Ling-ke Zhang
    Xiang-yang Zheng
    Defence Technology, 2018, 14 (05) : 422 - 425
  • [2] Experimental study on thermal decomposition kinetics of natural ageing AP/HTPB base bleed composite propellant
    Zhang, Ling-ke
    Zheng, Xiang-yang
    DEFENCE TECHNOLOGY, 2018, 14 (05): : 422 - 425
  • [3] Scatter of projectile affected by initial temperature of AP/HTPB composite base bleed propellant
    Zhang, Ling-Ke
    Yu, Yong-Gang
    Liu, Dong-Yao
    Lu, Xin
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2015, 23 (03): : 253 - 257
  • [4] Experimental study of material behavior of AP-HTPB base composite solid propellant
    Shin-Hoe Kim
    Yong-Taek Im
    Journal of Mechanical Science and Technology, 2019, 33 : 3355 - 3361
  • [5] Study on the thermal decomposition behavior of RDX/AP/HTPB propellant
    Chen, Pei
    Zhao, Feng-Qi
    Yin, Cui-Mei
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2002, 25 (02):
  • [6] Experimental study of material behavior of AP-HTPB base composite solid propellant
    Kim, Shin-Hoe
    Im, Yong-Taek
    JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2019, 33 (07) : 3355 - 3361
  • [7] Development of zirconium and potassium perchlorate igniter for AP/HTPB composite propellant base bleed grain
    Mukhtar, Amir
    Nasir, Habib
    Rashid, Badar
    Waheed, Hizba
    JOURNAL OF THERMAL ANALYSIS AND CALORIMETRY, 2019, 138 (06) : 3939 - 3947
  • [8] Development of zirconium and potassium perchlorate igniter for AP/HTPB composite propellant base bleed grain
    Amir Mukhtar
    Habib Nasir
    Badar Rashid
    Hizba Waheed
    Journal of Thermal Analysis and Calorimetry, 2019, 138 : 3939 - 3947
  • [9] EXPERIMENTAL STUDY OF TRANSIENT COMBUSTION CHARACTERISTICS OF AP/HTPB BASE BLEED PROPELLANT UNDER RAPID PRESSURE DROP
    Ye, Rui
    Yu, Yonggang
    Cao, Yongjie
    COMBUSTION SCIENCE AND TECHNOLOGY, 2015, 187 (03) : 445 - 457
  • [10] Burning rate of AP/HTPB base-bleed composite propellant under free ambient pressure
    Zhang, Lingke
    Tian, Ruyuan
    Zhang, Zhuwei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 62 : 31 - 35