Liquid Rocket Engine Turbopump Inducers (Paperback) (ISBN-13: 9781499234732)

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.

Author: National Aeronautics and Space Administr
ISBN-10: 1499234732
ISBN-13: 9781499234732
Publisher: Createspace Independent Publishing Platform
Language: English
Published: 04/28/2014
Pages: 114
Format: Paperback
Weight: 0.62lbs
Size: 11.02h x 8.50w x 0.24d