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Liquid Rocket Engine Turbopump Inducers

Contributor(s): National Aeronautics and Space Administr (Author)

ISBN: 9781499234732

Publisher: Createspace Independent Publishing Platform

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Pub Date: April 28, 2014

Lexile Code: 0000

Target Age Group: NA to NA

Physical Info: 0.24" H x 11.02" L x 8.50" W ( 0.62 lbs) 114 pages

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Reference | General

Descriptions, Reviews, etc.

Description: The inducer is the axial inlet portion of the turbopump rotor whose function is to raise the inlet head by an amount sufficient to preclude cavitation in the following stage. The inducer may be an integral part of the pump rotor or it may be mounted separately on the pump shaft upstream of the impeller.

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