首页 | 本学科首页   官方微博 | 高级检索  
     

双脉冲固体火箭发动机二次点火内视研究
引用本文:李江,肖育民,何国强,张伟青,杨雨阳,马国宝. 双脉冲固体火箭发动机二次点火内视研究[J]. 推进技术, 1998, 19(3): 61-64
作者姓名:李江  肖育民  何国强  张伟青  杨雨阳  马国宝
作者单位:西北工业大学航天工程学院,西安,710072,上海新力动力设备研究所,上海,200127
摘    要:利用X射线高速帝时荧屏分析(RTR)技术对双脉冲固体火箭发动机的二次点过程进行了内研究,通过对RTR图像的分析,弄清了隔板的打开模式以及塞子在一级燃烧室听运动规律,运用图像处理技术还获得了塞子飞出隔板后的平均速度及塞子与喷管碰撞后的反速度,这些结果为这种新型发动机的设计提供了实验依据。

关 键 词:双脉冲 固体火箭发动机 RTR 二次起动
修稿时间:1997-10-13

INNER VIEW OF DUAL PULSE SOLID ROCKET MOTOR DURING SECONDARY FIRING
Li Jiang,Xiao Yumin,He Guoqiang,Zhang Weiqing,Yang Yuyang and Ma Guobao. INNER VIEW OF DUAL PULSE SOLID ROCKET MOTOR DURING SECONDARY FIRING[J]. Journal of Propulsion Technology, 1998, 19(3): 61-64
Authors:Li Jiang  Xiao Yumin  He Guoqiang  Zhang Weiqing  Yang Yuyang  Ma Guobao
Affiliation:Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127;Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127;Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127;Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127;Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127;Shanghai Xin Li Power Equipment Research Inst ,Shanghai,200127
Abstract:The transient process inside dual pulse solid rocket motor during secondary firing was studied using a system of X ray real time radiography(RTR) technique The blowout pattern and the motion law of the plugs inside the first combustion chamber were found out by analyzing the RTR images By using advanced image processing techniques the mean flying velocities of the plugs after blowout and the reflection velocities of the plugs after impaction on the convergence section of the nozzle were obtained
Keywords:Dual pulse solid rocket motor  RTR technique +  Secondary start
本文献已被 维普 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF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