Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
Approved for public release; distribution is unlimited === The design and installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the high-pressure fuel turbopump of the Space Shuttle Main Engine, is reported. The specific article to be tested is the 'Alter...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/19733 |