期刊文献+

NEPE推进剂激光点火特性 被引量:15

Laser ignition of NEPE propellant
下载PDF
导出
摘要 采用CO2 激光点火系统 ,研究常压下NEPE推进剂中AP在点火过程中的作用 ,以及AP的表面积、燃速催化剂、初温、热流密度等因素与点火延迟时间的关系。结果表明 :与HMX相比 ,AP是缩短点火延迟时间的主要因素 ;初温对点火延迟时间的影响程度取决于热流量的大小 ,存在着所谓的“拉平效应”。而降低AP粒度 ,提高AP表面积 ,在初温大于 15℃时 ,有利于缩短点火延迟时间 ,而在小于 15℃时则相反 ; The effect of surface area of ammonium perchlorate(AP), initial temperature, heat fluxes and catalyst on the ignition delay time of NEPE propellant, which is a special nitromine composite propellant was examined in detail within a CO 2 laser ignition system. The results show that AP acts as a kind of trigger during ignition and is of more importance than HMX. There exists laser ignition thresholds, and the effect of initial temperature on ignition delay time is influenced by heat fluxes. This effect is more significant at lower heat fluxes. The large AP surface area benefits the decrease of ignition delay time when the initial temperature is higher than 15℃, while this effect will be realized by the relatively small AP surface area below 15℃. The addition of an effective catalyst can also shorten the ignition delay time by decreasing the reaction activation energy.
出处 《推进技术》 EI CAS CSCD 北大核心 2002年第2期172-175,共4页 Journal of Propulsion Technology
基金 国家自然科学基金资助项目 ( 5 97860 0 5 )
关键词 硝胺推进剂 激光点火 点火延迟 固体推进剂 NEPE Nitramine propellant Propellant ignition Laser ignition Ignition delay
  • 相关文献

参考文献9

  • 1Lim J U. Ignition dynamics of nitramine composite propellants under CO2 Laser heating[ R] . AIAA 87-0564.
  • 2Boggs. The role of gas reaction in deflagration-to-detonatoin transition[ C ]. 7 th Symposium on Detonation, 1981,1: 85 ~ 93.
  • 3Ktznetsov V T. Ignition of octagen by a light flux [ J ]. Fizika Goreniya i Vzryvia, 1977,13: 271 - 274.
  • 4Goveas S G. A study of the laser ignition of HMX/carbon black compositions[C]. Int. Annu. Conf. ICT 1999, 30, 22/1 -22/14.
  • 5Kashiwagi T.Ignition of a polymeric full in a hot oxidizing gas stream [ C ]. Thirteen International symposium on combustion, 1970,8:23 ~ 29.
  • 6Beckstead M W. A comparison of solid monopropellant combustion and modeling[R]. AIAA 97-0586.
  • 7金乐骥,李疏芬.复合固体推进剂中铝粉凝聚海绵模型[J].宇航学报,1989,10(3):25-32. 被引量:9
  • 8沙恒,李凤生,宋洪昌,陈舒林.超细高氯酸铵表面改性及对高燃速推进剂性能的影响[J].含能材料,1995,3(2):26-30. 被引量:19
  • 9Octavia. Chemical kinetics in the ignition delay of AP/NSAN/ INRT binder composition propellants[ C] . 27 th Internation Annual Conference of ICT, 1996,6.

二级参考文献4

  • 1金乐骥,兵工学报,1988年,2期,1页
  • 2李疏芬,航空动力学报,1987年,2卷,4期,342页
  • 3李疏芬,推进技术,1986年,3期,47页
  • 4郭申,1982年

共引文献26

同被引文献164

引证文献15

二级引证文献72

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部