Turbine performance mapping of the space-shuttle main engine high-pressure fuel turbopump

Approved for public release; distribution unlimited. === The redesign, data acquisition system installation, and software development for the cold-flow Turbine Test Rig is reported. The turbine tested was the Space Shuttle Main Engine High Pressure Fuel Turbopump first stage 'Alternate Turbopum...

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Bibliographic Details
Main Author: Greco, Philip Andrew
Other Authors: Hobson, Garth V.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/7566