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Liquid Rocket Engine Turbopump Inducers

Autor National Aeronautics and Space Administr
en Limba Engleză Paperback
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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Livrare economică 01-15 martie

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Specificații

ISBN-13: 9781499234732
ISBN-10: 1499234732
Pagini: 114
Dimensiuni: 216 x 279 x 6 mm
Greutate: 0.28 kg
Editura: CREATESPACE