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In the control of a missile, by means of gas jets lateral and missile a

机译:在导弹的控制中,通过侧面的气体喷射和导弹

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包括长方形的横截面,该横截面的最大尺寸至少包含在穿过纵轴l的平面中,即所述导弹1,而最小的尺寸为。所述倾斜部分至少近似垂直于该平面。

著录项

  • 公开/公告号FR2536720B1

    专利类型

  • 公开/公告日1985-03-15

    原文格式PDF

  • 申请/专利权人 SOCIETE NALE INDLE AEROSPATIALE;

    申请/专利号FR19820019996

  • 发明设计人

    申请日1982-11-29

  • 分类号B64C15/14;F42B15/18;

  • 国家 FR

  • 入库时间 2022-08-22 07:56:02

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