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此发明涉及一种采用喷气式发动机的导弹,此导弹装有推力矢量控制装置和气动控制装置,以施加横向力,可用相同的信号对这两个装置进行电控制。
The invention relates to a jet engine-powered missile equipped with a thrust vector control and a pneumatic control for exerting a lateral force to electrically control both devices with the same signal.