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APPARATUS AND METHOD FOR TESTING LIQUID PROPELLED ROCKET

机译:用于测试液体推进火箭的装置和方法

摘要

An apparatus for testing a liquid propelled rocket and associated method comprising a housing, a load cell assembly, a launcher assembly, a rocket assembly, and a base piston; the load cell assembly, the launcher assembly, the rocket assembly, and base piston situated within the housing; a hose to the launcher assembly or rocket assembly, supplying liquid or gas; the supply of gas and/or liquid pressurizes the rocket assembly and the launcher assembly, which may then be released to cause the rocket to exert a force in a direction opposite to the direction of the release of liquid and gas; the load cell adapted to measure the thrust of the rocket; the housing adapted to retain the released liquid; the base piston adapted to separate the launcher assembly from releasing liquid and gas, whereby the launcher assembly does not impede the release of water or air.
机译:一种用于测试液体推进的火箭和相关方法的装置,包括壳体,负载电池组件,发射器组件,火箭组件和基部活塞; 负载电池组件,发射器组件,火箭组件和位于壳体内的基部活塞; 软管到发射器组件或火箭组件,供应液体或气体; 然后,气体和/或液体的供应加压火箭组件和发射器组件,然后可以释放,然后可以释放,以使火箭施加力在与液体和气体释放方向相反的方向上的力; 称重块适于测量火箭的推力; 外壳适于保留释放的液体; 适于将发射器组件与释放液体和气体分开的基部活塞,由此发射器组件不妨碍水或空气的释放。

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