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 :
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