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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

Disclosed is an apparatus for testing a water rocket and a method for use thereof, the apparatus 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 all situated within the housing. A hose running from the exterior of the housing to the launcher assembly and/or the rocket assembly, whereby water or air may be supplied to the launcher assembly or the rocket assembly. The supply of air and/or water 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 water and air. The load cell is adapted to capture and record the thrust of the water rocket. The housing is adapted to retain the released water within the housing. The base piston is adapted to move the launcher assembly out of the way of the releasing water and air, whereby the launcher assembly does not impede the exit of the water or air that could result in inaccurate data.
机译:公开了一种用于测试水火箭的装置和用于其用于使用的方法,该装置包括壳体,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,火箭组件和基部活塞均位于壳体内。从壳体的外部到发射器组件和/或火箭组件的软管,由此水或空气可以被提供给发射器组件或火箭组件。空气和/或水的供应加压火箭组件和发射器组件,然后可以释放,以便使火箭沿与水和空气释放方向相反的方向施加力。称重传感器适于捕获并记录水火箭的推力。壳体适于在壳体内保持释放的水。底座活塞适于使发射器组件从释放水和空气的方式移动,由此发射器组件不会阻止可能导致数据不准确的水或空气的出口。

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