1) space missile
空间导弹
1.
The model of the space missile intercepting quickly was built and the orbit parameters were solved based on the theories of the orbit dynamics,second time and energies optimization,respectively.
根据轨道动力学的理论,建立空间导弹快速拦截模型,求解轨道参数。
2) missile attitude
导弹空间姿态<火>
3) outer-space missile
外层空间导弹
4) 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
5) 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。
6) airborne missile
空空导弹
1.
This paper narrated process techniques of copper infiltrated tungsten for airborne missile to fabricate jet vane.
论述了空空导弹推矢燃气舵用钨渗铜材料与制备工艺,以及在高温高速燃气流环境中的热强度、抗热震性、烧蚀率、抗热侵蚀性等关键性能和质量控制技术与要求,介绍了钨渗铜材料和工艺的新发展。
2.
By compareing the features and applicability of these two methods,it is suggested that these two methods should be separately used in different stages during the development of an airborne missile.
介绍了空空导弹上应用的两种环境应力筛选方法:常规环境应力筛选法和定量环境应力筛选法,并对两种方法的特点和适用性进行了比较,提出在空空导弹研制的不同阶段分别应用这两种环境应力筛选法的建议。
3.
Life(period of validity) is a key index for airborne missile system,as well for logistic support deployment and combat readiness.
寿命(有效期)是空空导弹的重要战技指标,对于战备和保障部署十分重要。
补充资料：MX导弹(见“和平卫士”导弹)
MX导弹(见“和平卫士”导弹)
MX missile
MX daodanMx导弹(Mx mis、ix。)见“和平卫士”导弹。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条