变形翼舵技术在导弹领域的应用需求及技术发展路线
The Application Requirements and Technological Development Route of Deformable Wing Rudder Technology in Missile Fields
姚重阳 1王晓鹏 2张海瑞 2雷豹 2夏艳2
作者信息
- 1. 清华大学国家卓越工程师学院,北京,100084;中国运载火箭技术研究院,北京,100076
- 2. 中国运载火箭技术研究院,北京,100076
- 折叠
摘要
采用变形翼舵技术可解决导弹对发射平台尺寸强约束问题,改善导弹升阻比及弹道末段机动性能,实现飞行全程气动外形最优,适应多任务作战需求.对国内外变形翼舵技术发展进行了概述,介绍了变形翼舵方案组成,分析了导弹对变形翼舵技术的需求,提出了单次阶跃变形、往复伸缩变形、柔性连续变形三阶段技术发展路线以及各阶段的关键技术,为变形翼舵技术在导弹武器领域的深入研究及应用提供了参考.
Abstract
The use of deformable wing rudder technology can solve the problem of strong constraints on the launch platform size of missiles,improve the lift to drag ratio and ballistic maneuverability of missiles,achieve optimal aerodynamic shape throughout the flight,and adapt to the needs of multi mission operations.The development of deformable wing rudder technology at home and abroad is summarized,the composition of deformable wing rudder scheme is briefly introduced.The missile's demand for deformable wing rudder technology is analyzed,and the development path of single step deformation,reciprocating expansion deformation,flexible continuous deformation and the key technologies of each stage are put forward.The research results provide a reference for the in-depth research and application of deformable wing rudder technology in the field of missile weapons.
关键词
变形翼舵/导弹/应用需求/发展路线/关键技术Key words
deformable wing rudder/missile/application requirements/development route/key technology引用本文复制引用
基金项目
国家自然科学基金联合基金(U20B2028)
出版年
2024
NETL
NSTL
万方数据