REG NASA-LLIS-0965-1995 Lessons Learned - Space Shuttle Main Engine (SSME) Turbopump Bearing Lubrication.pdf
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1、Lessons Learned Entry: 0965Lesson Info:a71 Lesson Number: 0965a71 Lesson Date: 1995-05-15a71 Submitting Organization: MSFCa71 Submitted by: Billy Cole / RetiredSubject: Space Shuttle Main Engine (SSME): Turbopump Bearing Lubrication Description of Driving Event: In the SSME, a small recirculation fl
2、ow is maintained by flowing the propellant through a bleed valve located at the main fuel valve to an overboard dump line or pumped back into the LH2 inlet. Recirculation flow of LOX is maintained by flowing LOX through a bleed valve located a the fuel preburner oxidizer valve to an overboard dump s
3、ystem. These recirculation flows have successfully eliminated gas pockets in the LH2 and LOX systems.Lesson(s) Learned: Recirculation flows of propellants can be used to pre-chill turbopumps to cryogenic temperatures and to eliminate gas pockets in the propellant feed system.Recommendation(s): Use r
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