反舰导弹喷口及尾焰辐射温度测量方法研究  

Analysis of Measurement Method of Radiation Temperature on Antiship Missile Nozzle and Wake Flame

作　　者：李桂芝[1] 衣同胜[1] 孙健[2] 

机构地区：[1]中国人民解放军92941部队91分队 [2]中国人民解放军92941部队93分队

出　　处：《现代防御技术》2016年第5期112-115,142,共5页Modern Defence Technology

摘　　要：针对反舰导弹飞行过程中红外辐射特性测量的难题,提出了一种红外目标辐射特性测量和标定方法,可实现对发动机尾喷口和尾焰辐射温度分布的测量。依据靶场环境特性,论证了红外光学系统的作用距离。红外辐射特性测量系统可实现反舰导弹飞行过程发动机工作状态的监控和辐射温度分布测量。According to the infrared measurement problem during antiship missile flight,the infrared radiation measurement and calibration method is proposed to measure the temperature distribution of antiship missile nozzle and wake flame. Based on environment characteristics of range,the infrared optical system operating range is demonstrated. The infrared radiation measurement system can monitor working condition of engine and measure temperature distribution.

关 键 词：测量方法 红外系统 辐射温度 尾焰 发动机 反舰导弹 

分 类 号：TJ761.14[兵器科学与技术—武器系统与运用工程] TJ760.6