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Hypothetical reentry thermostructural performance of space shuttle orbiter with missing or eroded thermal protection tiles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ko, William L. Quinn, Robert D. Gong, Leslie |
| Copyright Year | 2004 |
| Description | This report deals with hypothetical reentry thermostructural performance of the Space Shuttle orbiter with missing or eroded thermal protection system (TPS) tiles. The original STS-5 heating (normal transition at 1100 sec) and the modified STS-5 heating (premature transition at 800 sec) were used as reentry heat inputs. The TPS missing or eroded site is assumed to be located at the center or corner (spar-rib juncture) of the lower surface of wing midspan bay 3. For cases of missing TPS tiles, under the original STS-5 heating, the orbiter can afford to lose only one TPS tile at the center or two TPS tiles at the corner (spar-rib juncture) of the lower surface of wing midspan bay 3. Under modified STS-5 heating, the orbiter cannot afford to lose even one TPS tile at the center or at the corner of the lower surface of wing midspan bay 3. For cases of eroded TPS tiles, the aluminum skin temperature rises relatively slowly with the decreasing thickness of the eroded central or corner TPS tile until most of the TPS tile is eroded away, and then increases exponentially toward the missing tile case. |
| File Size | 1048641 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20040082249 |
| Archival Resource Key | ark:/13960/t2x39r896 |
| Language | English |
| Publisher Date | 2004-07-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Skin Temperature Non-biological Columbia Orbiter Uncontrolled Reentry Spacecraft Aluminum Space Shuttle Orbiters Wings Thermal Protection Tiles Ribs Supports Aerodynamic Heating Space Transportation System Aerothermodynamics Erosion Mach Number 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 |