某型火箭炮效力射诸元精度阈值研究  

Study on Accuracy of Firing Data in Fire for Effect of Rocket Launcher

作　　者：胡光宇 胡隆基 徐宁 李楠 施锦丹 HU Guangyu;HU Longji;XU Ning;LI Nan;SHI Jindan(No.63961 Unit, Beijing 100000, China)

机构地区：[1]63961部队

出　　处：《弹箭与制导学报》2018年第4期93-95,99,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中研究分析了某型火箭炮不经试射而直接进行效力射诸元精度阈值的意义,基于无控弹炮兵射击理论推导出某型火箭炮直接进行效力射诸元精度阈值计算模型,通过仿真实验对模型进行了验证,结合对某型火箭炮有无跟踪低空风雷达射击准确度数据的对比分析,指出通过加装低空风雷达,可以使火箭炮射击诸元精度达到直接效力射的要求,对确定某型火箭炮总体技术方案和实现该炮突出适应高原山地等特殊地形环境要求具有重要意义。This paper analyzed the threshold of firing data in fire for effect of rocket launcher without trial fire. The firing data model of rocket launcher to direct fire for effect without trial fire was built and verified by simulation experiments. The accuracy of firing data for rocket launcher can meet the requirement of the direct fire for effect with the help of low-level-wind radar, which is proved by the contrast experiments on firing accuracy of a rocket launcher with and without the low-level-wind radar. The experiment results can help to determine the whole technology program on rocket launcher and to improve its adaptive capacity for highland, mountain land, jungle, and island environments.

关 键 词：火箭炮 效力射 诸元精度 

分 类 号：TJ393[兵器科学与技术—火炮、自动武器与弹药工程]