Turbopumps for Liquid Rocket Engines
Author: Maynard L. Joe Stangeland
Publisher:
Published: 1992
Total Pages: 16
ISBN-13: 9781560912668
DOWNLOAD EBOOK →Author: Maynard L. Joe Stangeland
Publisher:
Published: 1992
Total Pages: 16
ISBN-13: 9781560912668
DOWNLOAD EBOOK →Author: Dieter K. Huzel
Publisher: AIAA
Published: 1992
Total Pages: 452
ISBN-13: 9781600864001
DOWNLOAD EBOOK →Author: National Aeronautics and Space Administration
Publisher: CreateSpace
Published: 2014-04-28
Total Pages: 112
ISBN-13: 9781499234732
DOWNLOAD EBOOK →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: NASA. Space Vehicle Design Criteria (Chemical Propulsion)
Publisher:
Published: 1971
Total Pages: 100
ISBN-13:
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