Hotfire testing of a SSME HPOTP with an annular hydrostatic bearing
Author:
Affiliation:
1. Rockwell International Corp., Rocketdyne Div., Canoga Park, CA
2. NASA, Marshall Space Flight Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2356
Reference15 articles.
1. Effects of Hydraulic Forces in Annular Pressure Seals on the Vibrations of Centrifugal Pump Rotors
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3. Turbulent hydrostatic thrust bearings. I - Bulk-flow analysis for performance and pneumatic hammer;32nd Joint Propulsion Conference and Exhibit;1996-07-01
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