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A method of suppressing elastic vibrations ROCKET PACKET DESIGN SCHEME

机译:一种抑制弹性振动的方法火箭弹设计方案

摘要

FIELD: transport.;SUBSTANCE: invention relates to aerospace engineering and may be used for killing elastic vibrations of clustered rocket bodies. Point-to-point gyros are mounted in three-degree-of-freedom suspensions to measure angular position of the rocket. Speed gyros are mounted on rocket body or on clusters to measure angular velocity of rocket or warhead. Law of controlling rocket engine nozzle and warhead deflection is generated. Rocket engine nozzles or warhead engine nozzles are deflected relative to rocket central body.;EFFECT: reduced stresses, rocket weight, increased payload, expanded operating performances.;5 dwg
机译:技术领域本发明涉及航空航天工程,并且可以用于消除集束的火箭弹的弹性振动。点对点陀螺仪安装在三自由度悬架中,以测量火箭的角位置。高速陀螺仪安装在火箭主体或机群上,以测量火箭或战斗部的角速度。产生了控制火箭发动机喷嘴和弹头偏转的规律。火箭发动机喷嘴或弹头发动机喷嘴相对于火箭中心部件发生偏斜;效果:应力减小,火箭重量增加,有效载荷增加,运行性能提高; 5 dwg

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