1)  Air-to-air missile
空-空导弹
2)  Air-to-air missile
空空导弹
1.
Research on the Control of Air-to-Air Missile at Large Angle of Off-Axis Shot;
空空导弹大离轴角发射条件下的控制研究
2.
Influence of double jet on air-to-air missile with lateral injection control;
双喷流对空空导弹直接力控制的影响
3.
Simulation research and overall design for SINS of air-to-air missile;
空空导弹捷联惯导系统总体设计与仿真研究
3)  Air to air missile
空空导弹
1.
Design of a 3-D adaptive fuzzy sliding mode guidance law for air to air missiles;
空空导弹三维自适应模糊滑模制导律设计
2.
Century scanning on the air to air missile research and development;
空空导弹研究与发展的世纪审视
3.
An air to air missile is affected by manifold shock and vibration environment when its captive carriage is flying.
空空导弹在挂飞过程中会遇到多种冲击和振动环境的作用,对导弹结构及其内部设备的性能影响不可忽视。
4)  AAM
空空导弹
1.
Research and Application of on Quick Simulation for the AAM with Complex Guidance;
复合制导空空导弹快速仿真研究与应用
2.
Modularization and Software Technology of AAM Fuze;
空空导弹引信模块化、软件化技术
3.
The jet TVC has become the most important key characters of the fourth generation AAM (air to air missile), by means of numerical simulation of jet TVC, This paper gives the thermal environment parameters, at the same time, we can get forces and torque of system control, and the influence to Solid Rocket Motor.
气动舵推力矢量技术已经成为先进红外格斗型空空导弹的标志性关键技术。
5)  anti-air-to-air missile
反空空导弹
6)  radar guided air-to-air missile
雷达型空-空导弹
1.
The characteristics of radar guided air-to-air missile and the design of missile simulation system are described and the integrated test process of missiles with aircraft equipments is introduced in the paper.
本文叙述了雷达型空-空导弹的特点和导弹仿真系统的设计,并介绍了导弹与机载设备的综合试验程序,最后对导弹截获目标概率进行了分析。
参考词条
补充资料:霍克对空导弹
Image:11727322477365368.jpg
霍克对空导弹

“霍克”短程对地导弹由美制“霍克”防空导弹改制而成。该弹制导方式为简单惯性制导,重量10,710 磅,长度39.8 英尺,射程约90 英里,动力装置为两级固体火箭发动机,战斗部装有300磅常规高爆炸药

说明:补充资料仅用于学习参考,请勿用于其它任何用途。