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MISSILE STEERING GEAR BY GASSY JET IN LATERAL DIRECTION AND MISSILE

机译:侧向和误导的盖斯射流导弹转向装置

摘要

System 7 for the control of a missile 1 by means of jets of gas f, having an incorporated gas 9a, 9b connected to at least a tuyere lateral 8, associated to a movable shutter controlling the flow of gas through said tuyere 8. According to the invention, this system is characterizes in that said tuyere 8 comprises an oblong cross section, the largest dimension of which is contained, of at least approximately in a plane passing through the longitudinal axis l - the said missile 1, whereas the smallest dimension of the said oblique section is directed, at least approximately, transversely to this plane.
机译:用于通过气体射流f控制导弹1的系统7,其具有结合到至少一个风口侧面8的结合的气体9a,9b,该气体9a,9b与控制通过该风口8的气流的可移动百叶窗相关。在本发明中,该系统的特征在于,所述风口8包括一个长方形的横截面,该横截面的最大尺寸至少大约在穿过纵轴l的平面中-所述导弹1,而其最小尺寸为。所述倾斜部分至少近似垂直于该平面。

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