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RDX粒度对改性双基推进剂性能影响 被引量:16

Effect of RDX Particle Size on Properties of CMDB Propellant
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摘要 实验研究了工业级RDX粒度对复合改性双基推进剂(CMDB)力学、燃烧及感度性能的影响。结果表明:黑索今平均粒径从92.02μm减小到17.35μm时,相应地固体推进剂高温最大抗张强度提高54%,低温延伸率提高85%;推进剂的燃速在不同压力下均有增加,最大增加11.5%;撞击感度特性落高增加5.1cm,摩擦感度爆炸百分率下降75%。 The effects of RDX particle size on properties of CMDB propellant including mechanical property,combustion property, sensitivity property and energy property were studied. The results show that when RDX particle size changes from 92.02 μm to 17.35 μm,correspondlng maximum tensile strength of CMDB propellant is enhanced by 54% at high temperature (50 ℃ ) and the elastic elongation is enhanced by 85% at low temperature ( -40 ℃ ) respectively. Meanwhile ,the burning rate of propellant at different pressure increases by 11.5% at its maximum. The characteristic height of impact sensitivity increases 5.1 cm,and the explosion percentage of friction sensitivity decreases by 75%.
出处 《含能材料》 EI CAS CSCD 2007年第3期220-223,共4页 Chinese Journal of Energetic Materials
关键词 军事化学与烟火技术 RDX 粒度 CMDB推进剂 military chemistry and pyrotechnical technology RDX particle size CMDB propellant
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参考文献10

  • 1Oberth A E,Bruenner R S.Binder filler interaction and propelllant mechanical properties[J].Transacation of Society of Theology,1965,9:165.
  • 2Oberth A E.Principle of strength reinforcement in filled rubbers[J].Rubber Chemistry and Technology,1967,40(5):1337-1363.
  • 3Gent A N.Detachment of an elastic matrix from a rigid spherical inclusion[J].Journal of Materials Science,1980,15:2884-2888.
  • 4冯增国,侯竹林.氧化剂粒度和含量变化对NEPE推进剂燃速和压力指数的影响[J].兵工学报,1995,16(1):7-9. 被引量:4
  • 5苏艳玲 孙育坤 李旭利.固体粒度对高能固体推进剂燃烧性能的影响.弹道学报,1998,(1):71-74.
  • 6袁嵩,汤卫红,李高春.复合推进剂的细观失效机理分析[J].固体火箭技术,2006,29(1):48-51. 被引量:21
  • 7Duterque J.Combustion mechanism of nitramine propellants with additives[R].AIAA 3253,1988.
  • 8Dehm Henry C.Composite modified double-base propellant with filler bonding agent[P].USP 4038115,1977.
  • 9张杏芬编译.国外火炸药原材料性能手册[M].北京:兵器工业出版社,1989.
  • 10刘玉存,王建华,安崇伟,于雁武.RDX粒度对机械感度的影响[J].火炸药学报,2004,27(2):7-9. 被引量:58

二级参考文献10

  • 1张宝坪,张庆明,黄风雷.爆轰物理学.北京:兵器工业出版社,1997.
  • 2[1]陈福梅.火工品设计[M].北京:北京理工大学84教研室,1991.
  • 3[2]Simpson R L,Urtiew P A, Ornellas D L, et al.CL-20 Performance exceeds that of HMX and its sensitivity is moderate[J]. Propellants Explosives Pyrotechnics,1997,22:249-255.
  • 4侯林法.复合推进剂[M].宇航出版社,1994..
  • 5Knauss W G.Fracture and failure at and near interface under pressure[R].ADA348939,1998.
  • 6Marur P R.Estimation of effective elastic properties and interface stress concentrations in particulate composites by unit cell methods[J].Acta.Materialia,2004,52:1263-1270.
  • 7Ghassemieh E.Micro-mechanical analysis of bonding failure in a particle-filled composite[J].Composite Science and Technology,2002,62:67-82.
  • 8张小宁 王卫民 徐更光.超细HMX和RDX撞击感度研究[J].火炸药学报,1999,22(1):1-3.
  • 9曾甲牙.丁羟推进剂拉伸断裂行为的扫描电镜研究[J].固体火箭技术,1999,22(4):69-72. 被引量:39
  • 10彭威,周建平,赵维昌,蒙上阳.复合固体推进剂应力分布的数值模拟及损伤萌生分析[J].固体火箭技术,2002,25(1):12-15. 被引量:12

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