一种空空导弹用直接力装置方案研究  

The Investigation of Lateral Thrust Set Project for Airborne Missile

作　　者：丁永强[1] 黄少波[1] 程翔[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《弹箭与制导学报》2011年第3期84-86,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：为了提高机动性和末端精确制导能力,未来的空空导弹有必要使用直接力装置。基于空空导弹的特点,空空导弹用直接力装置必须进行小型化设计,以减小重量、缩小体积。文中针对一种适用于空空导弹的直接力装置进行了方案研究,并对其进行了强度与内流场仿真计算,仿真结果表明该方案可行,为直接力装置将来在空空导弹上实际应用作了技术储备。In order to increase maneuverability and precision control ability, the future airborne missile requires the lateral thrust set. Based on the characteristic of airborne missile, the lateral thrust set for airborne missile must be a miniature design. （）ne later- al thrust set project for airborne missile was investigated, the intensity and inner flow field were simulated. The simulation indi cates the project is feasible and can serve as the technology repertory for airborne missile use of lateral thrust set.

关 键 词：空空导弹 直接力装置 方案研究 仿真计算 

分 类 号：TJ762.23[兵器科学与技术—武器系统与运用工程]