Monitoring device for combustion transient characteristics of solid rocket engine igniter

The invention belongs to the technical field of small tactical missile solid rocket engines, and particularly relates to a solid rocket engine igniter combustion transient characteristic monitoring device which is provided with a preformed hole and two glass windows. Pressure intensity data, infrare...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WANG SHUAIZHONG, TIAN XIAOTAO, YANG TAO, WANG CHEN, SU ZHENG, YU YUECHEN, PENG GUANWEI, XIAO BING, ZHANG QIONGFANG, XU YUAN, WANG SHAOZENG, ZHANG NAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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