炮射导弹

经参数优化的炮射导弹在给定的武装直升机各种航迹下，均可直接命中，脱靶量均小于1m，最大过载不超过可用过载。

The gun launched missile can directly hit the helicopters in the typical tracks , all the missdistances are less than 1 ? m and the maximum overload is less than available overload .

炮射导弹飞行可靠性试验法研究

Flight Reliability Test Method Study of cannon launched guided projectile

炮射导弹武器动态参数综合测试系统设计

Design of Integrated Test System for Dynamic Parameters of Gun-launched Missile Weapon

炮射导弹测试弹技术探讨

Investigation of the test projectile for the gun-launched missile

本文研究微机械陀螺仪及其在炮射导弹瞬时飞行姿态测量中的应用。

This paper studied on micromechanical gyros and its application on gun-launched missile attitude determination .

文中根据炮射导弹的射击特点，分析了炮射导弹落点精度的概念及其相关指标，提出了评定炮射导弹落点精度的方法。

A method to telemeter the attitude of the guided projectile on its terminal trajectory based on photogrammetry is introduced in this paper .

文中通过研究采用非金属材料弹带替代炮射导弹金属弹带材料。

In this paper , a research has been carried out that rotating band of the gun-lunched antitank missile can be replaced from metal material to nonmetallic material .

本文将介绍炮射导弹的发展史，研究炮射导弹测试弹的迫切性，以及我们对炮射导弹测试弹技术方案的初步探讨。

The paper describes the development history of the gun-launched missile and analyzes the significance to research the test projectile for the gun-launched missile . Besides , the paper puts forward the technique scheme for the gun-launched missile test projectile .

研究通过炮射反坦克导弹赋予坦克有限反武装直升机能力的可行性。

The feasibility of providing the tank a limited anti helicopter ability with gun launched missile is studied .