首页 | 本学科首页   官方微博 | 高级检索  
     

等离子体点火密闭爆发器中火药燃速特性的研究
引用本文:李海元, 栗保明, 李鸿志, 宁广炯, 王争论, 杨春霞. 等离子体点火密闭爆发器中火药燃速特性的研究[J]. 爆炸与冲击, 2004, 24(2): 145-150.
作者姓名:李海元  栗保明  李鸿志  宁广炯  王争论  杨春霞
作者单位:南京理工大学弹道国防科技重点实验室,江苏,南京,210094;南京理工大学弹道国防科技重点实验室,江苏,南京,210094;南京理工大学弹道国防科技重点实验室,江苏,南京,210094;南京理工大学弹道国防科技重点实验室,江苏,南京,210094;南京理工大学弹道国防科技重点实验室,江苏,南京,210094;南京理工大学弹道国防科技重点实验室,江苏,南京,210094
摘    要:等离子体与火药的作用规律是影响电热化学发射中能量利用效率的关键因素。研制了采用等离子体点火的密闭爆发器实验系统,对单基药在等离子体作用下的燃烧特性进行了研究。结果表明:等离子体点火可以显著缩短火药的点火延滞时间;实现有效点火的电能的最低阈值低于0.05kJ/g;输入电能可以显著增加火药的燃速。等离子体对所用单基药燃速的增强效果仅体现在电脉冲注入期间,但是随着电能输入的增加,逐渐显示出等离子体注入期后火药燃速增强的趋势。

关 键 词:爆炸力学  等离子体点火  密闭爆发器  电热化学发射
文章编号:1001-1455(2004)02-0145-06
修稿时间:2003-04-29

Propellant burn rate characteristics in closed bomb ignited with plasma
LI Hai-yuan,LI Bao-ming,LI Hong-zhi,NING Guang-jiong,WANG Zheng-lun,YANG Chun-xia. Propellant burn rate characteristics in closed bomb ignited with plasma[J]. Explosion and Shock Waves, 2004, 24(2): 145-150
Authors:LI Hai-yuan  LI Bao-ming  LI Hong-zhi  NING Guang-jiong  WANG Zheng-lun  YANG Chun-xia
Abstract:The interaction of plasma with propellant is the pivotal factor that influences energy efficiency of electrothermal chemical launch. An experimental system of closed chambeer with plasma igniter is developed. The characteristics of burn rate of single base propellant with the presence of plasma are investigated. Experimental results show that plasma ignition reduces propellant ignition delay markedly. The minimal threshold of ignition energy density is less than 0.05 kJ/g. The propellant exhibits enhanced burn rate with the increase of input electric energy. The enhancement of burn rate of single base propellant is only obvious in the period of electric pulse injection. When high electric energy injects into the chamber, there also exists tendency of regression rate enhancement after the plasma injection.
Keywords:mechanics of explosion  plasma ignition  closed chamber  electrothermal chemical launch  
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《爆炸与冲击》浏览原始摘要信息
点击此处可从《爆炸与冲击》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号