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METHOD OF SIMULATION OF CONDITIONS OF ROCKET LAUNCHING FROM SUBMARINE AND SYSTEM FOR ITS REALIZATION

机译:潜艇火箭发射条件的仿真方法及其实现系统

摘要

FIELD: determination of parameters of rocket launching from submarine in ground conditions. SUBSTANCE: hydrostatic pressure at launching depth, longitudinal resistance force, rocket weight and friction force at rocket motion in launching tube are simulated by solid-propellant rocket engine thrust on rocket mock-up placed in launching tube on ground supports. Engine thrust is directed against mock-up motion, and its magnitude is determined according to mathematical dependence. After engine delivers constant thrust mock-up ejection gas generator is actuated. System uses launching tube on ground supports, ejection gas generator, rocket mock-up with obturating belt and solid-propellant rocket engine. The latter is secured on mock-up with the aid of intermediate section connected to launching tube through blasting elements, and engine nozzle exit section is oriented in direction of mock-up ejection from launching tube. EFFECT: facilitated procedure. 2 cl, 3 dwg
机译:领域:确定地面条件下潜艇火箭发射的参数。物质:发射深度的静水压力,纵向阻力,火箭重量以及火箭在发射管运动时的摩擦力是通过固体推进剂火箭发动机在地面支架上放置在发射管中的火箭模型上的推力来模拟的。发动机推力是针对模拟运动的,其大小是根据数学依赖性确定的。发动机输出恒定推力后,启动模拟气体喷射气体发生器。该系统使用地面支撑物上的发射管,喷射气体发生器,带有密封带的火箭模型和固体推进剂火箭发动机。后者借助于通过爆破元件连接到发射管的中间部分固定在实体模型上,并且发动机喷嘴出口部分的方向与从发射管的实体模型喷射方向相同。效果:简化程序。 2 cl,3 dwg

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