首页> 外国专利> METHOD OF SIMULATION OF ROCKET LAUNCHING CONDITIONS FROM SUBMARINE LAUNCHER IN SUBMERGED POSITION AND SYSTEM FOR ITS REALIZATION

METHOD OF SIMULATION OF ROCKET LAUNCHING CONDITIONS FROM SUBMARINE LAUNCHER IN SUBMERGED POSITION AND SYSTEM FOR ITS REALIZATION

机译:水下位置发射器对火箭发射条件的仿真方法及其实现系统

摘要

FIELD: submarine launchers, in particular, launchers simulating a launching from a submarine in a submerged position. SUBSTANCE: simulated in a ground launcher on a rocket mock-up is the water pressure at the launching depth, buoyancy force, rocket weight and frictional force at motion in the launcher by means of the solid- propellant rocket engine, whose jet thrust is directed against the mock-up motion and the magnitude is determined from a mathematic relation. After the engine gains the preset power conditions the base pressure required for ejection is built up. The rocket launching simulation system represents a ground test rig, mock-up which the launching tube with the rocket mock-up positioned in it is secured on carrying supports. The rocket mock-up through a spacer is connected to the solid-propellant rocket engine, whose nozzle exit section is oriented in the direction of mock-up ejection. The spacer with the solid-propellant rocket engine is connected to the launcher by natural fasteners, the sum of the mock-up, rocket engine and spacer masses equals the rocket mass. The launching conditions simulation system functions as follows. The solid-propellant rocket engine is started in the assembled launcher, and after it gains the required thrust the gas generator is actuated. As a result, the pressure required for its ejection is built up on the mock-up base. The engine ends its operation after completion of operation of the gas generator, therefore, the conditions of a natural launching are completely simulated in the launcher during motion of the rocket mock-up. EFFECT: complete simulation of all loads acting on the rocket at launching from a submerged position, full safety of tests, considerably reduced expenditures connected with tests.
机译:领域:潜艇发射器,特别是模拟在水下位置从潜艇发射的发射器。物质:在火箭样机的地面发射器中模拟的是通过固体推进剂火箭发动机在发射器中的发射深度,浮力,火箭重量和运动时的摩擦力的水压,其喷射推力被定向相对于模型运动,幅度是根据数学关系确定的。发动机获得预设的功率条件后,将建立喷射所需的基本压力。火箭发射模拟系统代表一种地面测试装置,其上装有火箭模型的发射管固定在运载支架上。通过垫片的火箭模型连接到固体推进剂火箭发动机,该发动机的喷嘴出口部分朝向模型喷射的方向。带有固体推进剂火箭发动机的垫片通过天然紧固件连接到发射器,模型,火箭发动机和垫片的质量之和等于火箭的质量。发射条件模拟系统的功能如下。固体推进剂火箭发动机在组装好的发射器中启动,并在获得所需推力后启动气体发生器。结果,其排出所需的压力建立在模型基座上。发动机在气体发生器运行完成后结束其运行,因此,在火箭模型运动期间,发射器中的自然发射条件被完全模拟。效果:完全模拟从水下位置发射时作用在火箭上的所有载荷,充分的测试安全性,大大减少了与测试有关的支出。

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