Experimental Study on Cavitation Instabilities of Small Turbopump for Rocket Engine

A cavitation test was carried out for a fuel pump designated for a liquid rocket engine. The fuel enters the pump perpendicular to the direction of the shaft. Cavitation instabilities were investigated using an accelerometer installed on the pump casing and pressure transducers placed at the inlet a...

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Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2017, Vol.60(4), pp.230-234
Hauptverfasser:	HONG, Soonsam, CHOI, Changho
Format:	Artikel
Sprache:	eng
Schlagworte:	Accelerometers Cavitation Cavitation Instability Cavitation Surge Flow velocity Fluid flow Fuel Pump Liquid fuels Pumps Rocket engines Rockets Rotating Cavitation Transducers Turbopump
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