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Liquid hydrogen foil-bearing turbopumpThe testing and performance evaluation of a liquid hydrogen turbopump with the rotor supported by foil bearings is discussed. The objectives of the program were to demonstrate the long-life feature of a foil-bearing turbopump and to evaluate its operational characteristics. The demonstration has successfully shown the reliability, long life, and robust nature of foil-bearing turbopumps by operating for long periods of time, with many start and stop cycles and a wide speed range. It has also proven that foil-bearing turbopumps can start without total chilldown of the foil bearing, offering operational simplicity.
Document ID
19930066267
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gilbrech, Richard J.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Gu, Alston
(NASA John C. Stennis Space Center Bay Saint Louis, MS, United States)
Rigney, Tom
(NASA John C. Stennis Space Center Bay Saint Louis, MS, United States)
Saville, Marshall
(AlliedSignal Aerospace Systems & Equipment Torrance, CA, United States)
Rossoni, Mike
(McDonnell Douglas Aerospace Huntington Beach, CA, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 93-2537
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASME, AIAA, SAE, ASEE
Accession Number
93A50264
Distribution Limits
Public
Copyright
Other

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