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Evaluation of worn ssme low pressure liquid oxygen turbopump bearing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dufrane, K. F. Kannel, J. W. |
| Copyright Year | 1978 |
| Description | The larger of two ball bearings used to support the rotor of the low pressure liquid oxygen turbopump in each of the shuttle main engines was analyzed to identify the cause of severe internal wear. The actual operating loads were calculated along with their direction and length of time at each load based on the size and location of the race contact paths. It is suggested that the engine component design be modified to reduce bearing stress and enhance lubrication. |
| File Size | 3656727 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800007152 |
| Archival Resource Key | ark:/13960/t2n63bk3n |
| Language | English |
| Publisher Date | 1978-12-14 |
| Access Restriction | Open |
| Subject Keyword | Mechanical Engineering Stress Analysis Turbine Pumps Ball Bearings Wear Failure Analysis Liquid Oxygen Space Shuttle Main Engine Low Pressure Lubrication Loads Forces Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |