Analysis of agglomerate size from burning aluminized AP/RDX/HTPB propellants in quench bomb

被引:12
|
作者
Liu, TK
Hsieh, CF
机构
[1] Chemical System Research Division, Chung Shan Inst. Sci. and Technol., Lungtan
关键词
D O I
10.2514/3.24133
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:995 / 998
页数:4
相关论文
共 36 条
  • [1] Calculation on burning rate characteristics of AP/RDX/HTPB propellants
    Natl Univ of Defense Technology, Changsha, China
    Tuijin Jishu, 4 (75-79):
  • [2] Very-High-Pressure Burning Rates of Aluminized and Nonaluminized AP/HTPB-Composite Propellants
    Dillier, Catherine A. M.
    Petersen, Erica D.
    Sammet, Thomas
    Petersen, Eric L.
    JOURNAL OF PROPULSION AND POWER, 2021, 37 (05) : 693 - 700
  • [3] 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
  • [4] COMBUSTION CHARACTERISTICS OF AP HTPB PROPELLANTS WITH BURNING RATE MODIFIERS
    KRISHNAN, S
    JEENU, R
    JOURNAL OF PROPULSION AND POWER, 1992, 8 (04) : 748 - 755
  • [5] EFFECT OF ACCELERATION ON THE BURNING RATE OF HTPB COMPOSITE ALUMINIZED SOLID PROPELLANTS.
    Zhang, Ruzhoug
    Li, Baojiangi
    Zheng, Xiaoping
    Binggong Xuebao/Acta Armamentarii, 1988, (02): : 17 - 23
  • [6] Burning of aluminized solid rocket propellants: from micrometric to nanometric fuel size
    De Luca, Luigi T.
    THEORY AND PRACTICE OF ENERGETIC MATERIALS, VOL VII, 2007, : 277 - 289
  • [7] Iron Nanoparticle Additives as Burning Rate Enhancers in AP/HTPB Composite Propellants
    Styborski, Jeremy A.
    Scorza, Matthew J.
    Smith, Melissa N.
    Oehlschlaeger, Matthew A.
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2015, 40 (02) : 253 - 259
  • [8] Effects of particle size and content of RDX on burning stability of RDX- based propellants
    Wang, Bin-bin
    Liao, Xin
    DeLuca, Luigi T.
    He, Wei-dong
    DEFENCE TECHNOLOGY, 2022, 18 (07) : 1247 - 1256
  • [9] Effects of particle size and content of RDX on burning stability of RDX-based propellants
    Binbin Wang
    Xin Liao
    Luigi TDe Luca
    Weidong He
    Defence Technology, 2022, 18 (07) : 1247 - 1256
  • [10] Effects of particle size and content of RDX on burning stability of RDX-based propellants
    Bin-bin Wang
    Xin Liao
    Luigi T.De Luca
    Wei-dong He
    Defence Technology , 2022, (07) : 1247 - 1256