Liquid Rocket Engine Turbopump Inducers

By National Aeronautics and Space Administration

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... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1499234732
• ISBN13: 9781499234732
• Release Date: April 2014
• Publisher: Createspace Independent Publishing Platform
• Length: 114 Pages
• Weight: 0.62 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"