DocumentCode
2342483
Title
The Design of the Monitoring Circuit for the Rocket Ignition Process
Author
Zeling, Liu ; Yongfeng, Ren ; Shengkun, Li ; Huijing, Li
Author_Institution
Nat. Key Lab. for Electron. Meas. Technol., North Univ. of China, Taiyuan, China
Volume
2
fYear
2010
fDate
18-20 Dec. 2010
Firstpage
660
Lastpage
663
Abstract
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.
Keywords
avionics; network synthesis; rocket engines; monitoring circuit design; rocket ignition process; space rocket engine; Monitoring Circuit; Rocket Engine; Safe Ignition;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Manufacturing and Automation (ICDMA), 2010 International Conference on
Conference_Location
ChangSha
Print_ISBN
978-0-7695-4286-7
Type
conf
DOI
10.1109/ICDMA.2010.221
Filename
5701493
Link To Document