Effect of TMOs combustion characteristics of aluminum-magnesium fuel-rich propellant at low pressure

被引:0
|
作者
Zhang, Wei
Zhu, Hui
Xia, Zhi-Xun
机构
来源
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2002年 / 25卷 / 03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] Analyzing the condensed-phase reaction of the combustion of fuel-rich solid propellant based on boron in low pressure
    Wang, YH
    Cai, H
    Wang, MJ
    Xu, T
    Theory and Practice of Energetic Materials, Vol 6, 2005, : 607 - 610
  • [22] Characterization Methods of Combustion Properties of Aluminummagnesium Fuelrich Propellant at Low PressureChinese Full Text
    张炜
    朱慧
    含能材料, 2002, (03) : 125 - 127
  • [23] Numerical simulation of deposition for aluminum/magnesium-loaded fuel-rich propellant ducted rockets
    Wang, De-Quan
    Xia, Zhi-Xun
    Hu, Jian-Xin
    Guo, Jian
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (02): : 445 - 449
  • [24] COMBUSTION CHARACTERISTICS OF GAP-COATED BORON PARTICLES AND THE FUEL-RICH SOLID-PROPELLANT
    SHYU, IM
    LIU, TK
    COMBUSTION AND FLAME, 1995, 100 (04) : 634 - 644
  • [25] Thermal reaction characteristics of the boron used in the fuel-rich propellant
    Liu, Lin-lin
    He, Guo-qiang
    Wang, Ying-hong
    JOURNAL OF THERMAL ANALYSIS AND CALORIMETRY, 2013, 114 (03) : 1057 - 1068
  • [26] Thermal reaction characteristics of the boron used in the fuel-rich propellant
    Lin-lin Liu
    Guo-qiang He
    Ying-hong Wang
    Journal of Thermal Analysis and Calorimetry, 2013, 114 : 1057 - 1068
  • [27] Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant
    Rathi, Nikunj
    Ramakrishna, P. A.
    JOURNAL OF PROPULSION AND POWER, 2017, 33 (05) : 1207 - 1217
  • [28] Experimental study of combustion properties of magnesium-aluminum alloys in solid fuel-rich propellants
    Xiuyou, Xiao
    Yuling, Wang
    Yanfeng, Liu
    Zhuanjian, Liu
    THEORY AND PRACTICE OF ENERGETIC MATERIALS, VOL VII, 2007, : 592 - 594
  • [29] Fuel-rich Combustion with AP added Propellant in a Staged Hybrid Rocket Engine
    Lee, Dongeun
    Lee, Changjin
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2016, 44 (07) : 576 - 584
  • [30] Research on combustion efficiency of boron based fuel-rich propellant in the oxygen bomb
    Wang, Ying-Hong
    He, Chang-Jiang
    Li, Bao-Xuan
    Liu, Lin-Lin
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2012, 35 (06): : 782 - 786