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叙述了由火箭发动机推进的照明弹战斗部的降落伞开伞系统,该系统使用的紧凑的两级伞系统包括:主伞套内安置的主伞和阻力伞套内安装的阻力伞,主伞包和阻力伞紧挨着分开放置在战斗部内。拉绳把阻力伞包和发动机可分离地联在一起,而一个栓绳把阻力伞包和主伞相联,因此,当火箭发动机从战斗部分离时,拉出主伞包之前阻力伞先从战斗部拉出,当阻力伞展开时阻力伞罩仍连在拉绳上,起偏转板的作用,产生的径向力作用在火箭发动机上,以防止它与战斗部碰撞。
Describes a parachute-opening system for a rocket-propelled warhead of a rocket engine. The system uses a compact two-stage umbrella system that includes a main parapet installed in a main parapet and a resistance umbrella installed in the parachute, Drag the umbrella next to each other in the warhead. The pull cord separates the drag umbrella from the engine and a tether connects the drag umbrella to the main parachute. Therefore, when the rocket motor is detached from the warhead, the drag umbrella pulls away from the main parachute War Department pulled out, when the resistance umbrella unfolded resistance umbrella cover is still connected to the rope, the role of the deflection plate, the resulting radial force on the rocket engine to prevent it from collisions with the warhead.