一种改进型远程火箭弹发动机点火装置  

An Improved Ignition Device for Long-range Rocket Engine

作　　者：杨青山 赵成文 刘波 李泽亨 王旭兵 尚育生 Yang Qingshan;Zhao Chengwen;Liu Bo;Li Zeheng;Wang Xubing;Shang Yusheng(No.3 Military Representative Office in Taiyuan District,Taiyuan 030008,China;Technology Department,Jiangyang Co.,Ltd.of Jinxi Industries Group Co.,Ltd.,Taiyuan 030041,China;Scientific Research Institute,Shanxi Jindong Chemical Plant,Yangquan 045000,China)

机构地区：[1]驻太原地区第三军事代表室,太原030008 [2]晋西工业集团江阳公司技术部,太原030041 [3]山西晋东化工厂科研所,山西阳泉045000

出　　处：《兵工自动化》2022年第9期83-86,92,共5页Ordnance Industry Automation

摘　　要：针对火箭弹作战远程化的装备发展趋势,对适用于远程火箭弹发动机的点火装置设计进行改进。对满足其功能要求的结构设计、数值计算、技术环节、功能验证等进行研究,介绍某改进型远程火箭弹固体火箭发动机点火装置的设计和试验情况。结果表明,该研究的相关改进和试验可为后续系列火箭弹发动机点火装置的设计提供参考。Aiming at the equipment development trend of long-range rocket,the design of ignition device for long-range rocket engine was improved.The structural design,numerical calculation,technical links and functional verification to meet the functional requirements were studied.The design and test of the ignition device of certain type improved long-range rocket solid rocket motor were introduced.The results show that the related improvement and test can provide a reference for the design of the ignition device of the following series of rocket motors.

关 键 词：设计 点火装置 改进 功能验证 

分 类 号：TJ415[兵器科学与技术—火炮、自动武器与弹药工程]