Turbopumps for Liquid Rocket Engines
Author : Maynard L. Joe Stangeland
Publisher :
Page : 16 pages
File Size : 49,19 MB
Release : 1992
Category : Technology & Engineering
ISBN : 9781560912668
Author : Maynard L. Joe Stangeland
Publisher :
Page : 16 pages
File Size : 49,19 MB
Release : 1992
Category : Technology & Engineering
ISBN : 9781560912668
Author :
Publisher :
Page : 132 pages
File Size : 34,2 MB
Release : 1978
Category : Jet pumps
ISBN :
Author : R. E. Burcham
Publisher :
Page : 174 pages
File Size : 35,82 MB
Release : 1978
Category : Fuel pumps
ISBN :
Author : L. K. Severud
Publisher :
Page : 140 pages
File Size : 15,46 MB
Release : 1972
Category : Liquid propellant rockets
ISBN :
Author :
Publisher :
Page : 176 pages
File Size : 45,11 MB
Release : 1974
Category :
ISBN :
Author : Dieter K. Huzel
Publisher : AIAA
Page : 452 pages
File Size : 35,33 MB
Release : 1992
Category : Liquid propellant rocket engines
ISBN : 9781600864001
Author :
Publisher :
Page : 124 pages
File Size : 41,8 MB
Release : 1973
Category :
ISBN :
Author : R. B. Furst
Publisher :
Page : 124 pages
File Size : 19,68 MB
Release : 1973
Category : Centrifugal pumps
ISBN :
Author : National Aeronautics and Space Administration
Publisher : CreateSpace
Page : 112 pages
File Size : 17,24 MB
Release : 2014-04-28
Category :
ISBN : 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 : NASA. Space Vehicle Design Criteria (Chemical Propulsion)
Publisher :
Page : 100 pages
File Size : 32,80 MB
Release : 1971
Category :
ISBN :