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A device for stabilizing a missile, in particular is driven by a reaction

机译:一种用于稳定导弹的装置,特别是由反作用力驱动的装置

摘要

P device for stabilizing a missile, in particular, propelled by reaction, on its path during the initial phase of its flight by means of the force of a cable acting on the missile, in particular on its rear central part, and causing the stabilizers in the case of the longitudinal axis of the missile with respect to the tangent to the trajectory, the said force being generated by a brake on the cable. / p & & p & as a brake cable, it is provided a calibrated die installed in the missile, k, in particular at the center of its rear part 2, or on the launching ramp a, this die having a very narrow cross section whose diameter, in order to produce the braking force necessary, is smaller than that of the braking cable 6 used in the die. / p
机译:

一种装置,用于稳定,特别是通过在导弹飞行初始阶段由反作用力推动的导弹,该装置借助作用在导弹上,特别是在其后部中央部分上的电缆的力来使导弹稳定在导弹的纵轴相对于轨迹的切线的情况下为稳定器,所述力由电缆上的制动器产生。 & &作为制动拉索,提供了一个安装在导弹k中的校准模具,特别是在其后部2的中心,或者安装在发射坡道a上,该模具的横截面非常狭窄,以便产生所需的制动力,小于在模具中使用的制动力6。

著录项

  • 公开/公告号FR2422993B1

    专利类型

  • 公开/公告日1983-06-17

    原文格式PDF

  • 申请/专利权人 MESSERSCHMITT BOLKOW BLOHM GMBH;

    申请/专利号FR19790008989

  • 发明设计人

    申请日1979-04-09

  • 分类号G05D1/08;F42B15/04;

  • 国家 FR

  • 入库时间 2022-08-22 10:02:03

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