1) missile trigger mechanism
导弹发射机构
1.
A automatic testing device for the missile trigger mechanism controlled by 8031 single chip microcomputer is presented, its principle of the work and software hardware design are introduced.
介绍了一种由 80 31单片机控制的导弹发射机构的自动检测装置 ,详述了其组成、工作原理和软硬件设计方法。
2) Mobile missile launcher
导弹机动发射车
3) missile launch
导弹发射
1.
The seeker aim angles are two of air to air missile launch and control parameters.
空空导弹导引头角预定是重要的导弹发射控制参数，其有效的计算精度分析，是导弹可靠截获和跟踪目标的重要保证。
4) missile launching
导弹发射
1.
A virtual experiment system simulation modeling of a certain missile launching process is built on the MSC Adams platform according to its physical model.
以某导弹发射过程为物理原型,在MSCAdams环境下建立对应的虚拟试验系统仿真计算模型,使用多组不同的参数进行仿真计算,获得较为完备的虚拟试验数据及其不同的参数对性能影响的数据,为该型导弹的物理样机设计提供一定的基础技术支持。
5) Ejection Mechanism
弹射机构
1.
The Structure Design and Dynamic-parameter Simulation of a Sort of Missile Ejection Mechanism;
某型弹射机构结构设计计算及动态参数仿真
2.
The whole mathematical model of a missile ejection mechanism was consisted of the equivalence dynamic model of the mechanism and the mathematical model of its nitrogen cylinder which was built based on the law of thermodynamics.
根据热力学运动定律建立的氮气作动筒的数学模型与机构的等效动力学模型耦合起来,组成了整个弹射机构的数学模型。
3.
Based on the requirement of developing and designing the airborne ejection device,a new ejection mechanism is ac- quired.
根据发射装置产品研制与设计生产的需要,设计了一种新的弹射机构。
6) ejection device
弹射机构
1.
A model of blank cartridge ejection device was established and the ejection and restoration processes described.
本文建立了采用气体驱动弹射—回收的抛放弹弹射机构的数值计算模型 ,用经典内弹道和气体动力学理论分析了火药弹燃烧、弹射活塞完全推离悬挂物 (导弹或炸弹 )并回缩到初始状态的整个过程。
2.
A numerical model for suspender ejection device with the powder gas of blank cartridge as driving energy is established.
建立采用抛放弹火药燃气作为工作能源的挂弹钩弹射机构的数值计算模型,对抛放弹燃烧,弹射活塞非对称工作,直至推离悬挂物(导弹或炸弹)的整个动态过程进行了模拟计算。
3.
An optimum design model of ejection device with blank cartridge is established based on the theories of interior ballistics, gas dynamics and optimization.
该文应用内弹道、气体动力学和优化设计理论建立了抛放弹弹射机构的优化设计模型。
补充资料：导弹机动发射(见导弹发射方式)
导弹机动发射(见导弹发射方式)
maneuverable launching of missile
算薰;笙簌巍骂 able launching 式。
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