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DEVICE FOR TWO-STAGE ROCKET STAGES SEPARATION

机译:火箭两阶段分离装置

摘要

FIELD: weapon and ammunition.;SUBSTANCE: device for two-stage rocket stages separation is made in the form of a steering control mechanism mounted on the rocket body with a possibility of two links separation (at the time of rocket stages separation). One link is kinematically connected with the aerodynamic steering wheel shaft, which is placed on the main rocket stage. The other link is connected to the gas rudder, which is placed on the starting stage. The link, connected with the aerodynamic steering wheel shaft, contains a rocker, hingedly mounted on the main stage, at the ends of which two grooves are made. One groove is intended for placement of a finger, rigidly fixed on the lever of the aerodynamic handlebars steering wheel shaft. The other groove is intended for placement of a finger rigidly fixed to the rocker of the link connected to the gas rudder, mounted on the starting stage. At that, the rocker ends are pivotally connected to a pair of rods pivotally connected to the gas rudder rocker.;EFFECT: simplified design of the device for two-stage rocket stages separation with a possibility to disengage the links of the steering control mechanism.;2 dwg
机译:领域:武器和弹药。实体:用于火箭两级分离的装置是以转向控制机构的形式制成的,该转向控制机构安装在火箭主体上,有可能两个连杆分离(在火箭级分离时)。一个连杆与气动方向盘轴在运动学上相连,该方向盘轴位于主火箭级上。另一连杆连接至放置在起步阶段的气体舵。与空气动力学方向盘轴连接的连杆包含一个摇杆,该摇杆铰接安装在主平台上,在其两端设有两个凹槽。一个凹槽用于放置手指,该凹槽牢固地固定在空气动力学方向盘方向盘轴的杆上。另一个凹槽用于放置一个手指,该手指牢固地固定在连杆的摇杆上,该连杆与气体舵连接,并安装在起步台上。此时,摇臂端部可枢转地连接到一对枢轴连接到气体舵摇杆的杆上。效果:用于两级火箭级分离的设备的简化设计,可能会分离转向控制机构的连杆。 ; 2 dwg

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