The Design of the Monitoring Circuit for the Rocket Ignition Process

摘要：

In ignition process of the space rocket engine, design of the monitoring circuit is very important .If the monitoring circuit can not reliably work, separation of the rocket engine will be greatly affected, thereby the safe ignition of the rocket engine will be affected. In this paper, aiming at the real problem in the ignition process, the monitoring circuit has been improved on the design . A large number of tests showed that the improved monitoring circuit can run reliably. In addition, the safe ignition for the rocket engine can be realized by the application of it.

关键词： Rocket Engine Monitoring Circuit Safe Ignition

作者: Liu Zeling Ren Yongfeng Li Shengkun Li Huijing

作者单位: National Key Laboratory for Electronic Measurement Technology, North University of China, Taiyuan,Shanxi,030051 ,China

会议类型: 国际会议

会议名称: 2010 International Conference on Digital Manufacturing and Automation(2010 数字制造与自动化国际会议 ICDMA 2010)

会议地点: 长沙

会议语种:英文

页码: 660-663

在线出版日期: 2010-12-18（万方平台首次上网日期，不代表论文的发表时间）