防空多管火箭炮位置伺服系统负载特性分析  

Loading Characteristic Analysis of Position Servo System of Multiple Launch Rocket System for Air Defense

作　　者：朱玉川[1] 马大为[1] 李志刚[1] 乐贵高[1] 

机构地区：[1]南京理工大学,南京210094

出　　处：《弹箭与制导学报》2005年第4期66-67,79,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中依据某小口径多管火箭炮机械结构及防空反导的战术要求,对影响多管火箭炮位置伺服系统性能的摩擦力矩、不平衡力矩、燃气流冲击力矩以及转动惯量的变化规律等进行了详细的分析,为多管火箭炮位置伺服系统的进一步研究提供了依据和基础。In this paper, basis on mechanical s tactical demand of air defense and antimissile, it moment of burning gas flow and variable rule of position servo system of multiple launch rocket tructure of certain minor caliber multiple launch rocket system and is analyzed in detail that friction torque, unbalanced moment, impact moment of inertia, which provide the foundation for more research of system

关 键 词：防空反导 多管火箭炮 不平衡力矩 燃气流 转动惯量 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]