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Ssme fuel preburner injector characterization
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hutt, John J. |
| Copyright Year | 1993 |
| Description | A project has been initiated at the Marshall Space Flight Center to determine if preburner inter- or intra-element mixture ratio maldistributions are the cause of temperature variations in the Space Shuttle Main Engine (SSME) High Pressure Fuel Turbopump (HPFTP) turbine inlet region. Temperature nonuniformity may contribute to the many problems experienced in this region. The project will involve high pressure cold-flow testing and Computational Fluid Dynamics (CFD) modeling. |
| File Size | 215370 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940018564 |
| Archival Resource Key | ark:/13960/t2p60gv13 |
| Language | English |
| Publisher Date | 1993-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Temperature Measurement Turbine Pumps Preburners Injectors Computational Fluid Dynamics Mixing Ratios Temperature Gradients Space Shuttle Main Engine Cracking Fracturing Cold Flow Tests Fuel Injection Turbines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
