某型远程火箭炮训练模拟弹弹道特性研究  

Study on the Trajectory Properties of Long-Range Rocket Training Simulation Projectile

作　　者：王世界 刘玉文 

机构地区：[1]陆军军官学院,合肥230031

出　　处：《四川兵工学报》2013年第8期56-57,72,共3页Journal of Sichuan Ordnance

摘　　要：某型远程火箭炮采用122 mm火箭弹实弹作为训练模拟弹,由于远程火箭炮与122 mm火箭炮定向管长度的不同,导致它们的弹道特性有所差异。对两者弹丸出定向管管口附近同一位置的速度、弹道倾角和地面风修正量等弹道特性进行分析研究,得出了不能用现有122 mm火箭炮射表决定远程火箭炮训练弹射击诸元的结论。Long-range rocket with 122 mm rocket projectile are used as training simulation missiles, be-cause of the long-range rocket with 122 mm rocket launcher tube of different length, it leads to that the ballistic characteristics of them are different. Analyzing from both the directional pipe near the same loca-tion speed, trajectory angle and surface wind correction and ballistic characteristics, it cannot use the ex- isting 122 mm rocket firing table to determine the long-range rocket gun training missile firing.

关 键 词：训练模拟弹 弹道倾角 地面风修正量 弹道特性 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]