rocket igniter

A hybrid rocket motor using this igniter was tested. The experiment results demonstrated that this new igniter can successfully start the N2O/ PMMA hybrid motor.

试验表明，在催化剂被加热到400~600℃左右后，该点火器可以成功启动N2O/有机玻璃（PMMA）混合火箭发动机。

Nondestructive Inspection Principle and Failure Criteria of the Electric Igniter in Rocket

火箭弹发动机电点火具无损检测原理与失效判据分析

Comparative Analysis of Several Types of Igniter for Rocket Projectile

几种火箭弹点火具的对比研究

Taking aft-end igniter design for a rocket motor for example, design methods for ignition sequence, amorce quantity estimation and nozzle closure were described respectively.

以某型号发动机尾部点火设计为研究对象，对点火序列设计、点火药量的估算、喷管堵片的设计方法进行了阐述。