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.
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