A kind of igniter has been designed for minute solid rocket motor. Many tests have been done to determine the ignition characteristics of minute solid rocket motor. A concept of initial ignition pressure has been introduced the principal principle which effected ignition delay time scatter has been found and determined the ignition scheme satisfying the demand for ignition performance of minute solid rocket motor determined.
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孙丕忠,秦子增,张晓今,等.微小型固体火箭发动机点火特性试验. Test Research on the Ignition Characteristics of Minute Solid Rocket Motor[J].国防科技大学学报,2000,22(5):23-25.