Study of combustion characteristics of RDX/HTPB propellant

被引：0
|
作者：
Tu, Yongzhen
Wang, Chaozhen
机构：
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 1995年 / 18卷 / 02期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [21] 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
  • [22] Emission imaging of AP/HTPB propellant sandwich combustion
    Chorpening, BT
    Brewster, MQ
    COMBUSTION SCIENCE AND TECHNOLOGY, 2002, 174 (04) : 39 - 60
  • [23] Effect of size grading of NC powder on the combustion characteristics of RDX-CMDB propellant
    Guan, Dalin
    Liu, Xiaogang
    Chen, Xueli
    Zhang, Shuangjian
    Huozhayao Xuebao/Chinese Journal of Explosives & Propellants, 21 (04):
  • [24] Molecular Simulations of HTPB/Al/AP/RDX Propellants Combustion
    Chu Q.-Z.
    Fu X.-L.
    Zheng X.-M.
    Liu J.-L.
    Chen D.-P.
    Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2024, 47 (03): : 254 - 261
  • [25] Combustion mechanism of an RDX-based composite propellant
    De Luca, L
    Cozzi, F
    Germiniasi, G
    Ley, I
    Zenin, AA
    COMBUSTION AND FLAME, 1999, 118 (1-2) : 248 - 261
  • [26] Role of bimodal RDX in LOVA gun propellant combustion
    Joshi, MM
    Dayanandan, CR
    Pillai, AGS
    Gandhe, BR
    Karir, JS
    DEFENCE SCIENCE JOURNAL, 1998, 48 (03) : 317 - 321
  • [27] Characteristics of HTPB propellant with high solid contents
    School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
    Hanneng Cailiao, 2007, 1 (42-46):
  • [28] Effects of DC Electric Field on Combustion Characteristics of AP/HTPB/Al Composite Solid Propellant
    Huang, Xing
    Gan, Yun-Hua
    Ao, Wen
    Zhao, Ming-Tao
    Luo, Yan-Lai
    Jiang, Zheng-Wei
    Chen, Ning-Guang
    Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (01):
  • [29] Study of catalyzing thermal decomposition and combustion of AP/HTPB propellant with nano Cu/CNTs
    National Special Superfine Powder Engineering Research Center, Nanjing University of Science and Technology, Nanjing 210094, China
    Binggong Xuebao, 2008, 9 (1029-1033):
  • [30] Study on combustion properties of HTPB propellant containing nitramine under high and low pressure
    Jia, Xiao-Feng
    Su, Chang-Yin
    Lu, Gong-Lian
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2002, 25 (01):
12345