平衡抛射式火箭弹筒口测速技术研究  

The Technology of Measuring Muzzle Velocity of Individual Equilibrium Launch Rocket

作　　者：姚家红[1] 才伟 张明宏[1] 

机构地区：[1]安徽东风机电科技股份有限公司,合肥230041 [2]南京军代局驻合肥地区军代室,合肥230041

出　　处：《价值工程》2016年第14期193-194,共2页Value Engineering

摘　　要：本文提出一种基于初、次级线圈电磁耦合的平衡抛射式火箭弹初速测量方法,给出了软硬件实现方案,射击回收试验验证了该方法的可行性。This paper presents an implementation method of measuring muzzle velocity for individual equilibrium launch rocket based on inductive coupler between coils. The principle, the key technology and the circuit of the measuring method are described. The experiment results show the method is realizable.

关 键 词：测速 火箭弹 平衡抛射 

分 类 号：E927[军事—军事装备学]