| タイトル | Task 4 supporting technology. Part 1: Detailed test plan for leading edge tile development. Leading edge material development and testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950021837 |
| 著者（英） | Hogenson, P. A.; Hinkle, Karrie; Staszak, Paul |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1995-05-30 |
| 言語 | eng |
| 内容記述 | This task develops two alternative candidate tile materials for leading edge applications: coated alumina enhanced thermal barrier (AETB) tile and silicone impregnated reusable ceramic ablator (SIRCA) tile. Upon reentry of the X-33/RLV space vehicle, the leading edges experience the highest heating rates and temperatures. The wing leading edge and nose cap experience peak temperatures in the range 2000 to 2700 F. Replacing reinforced carbon-carbon (RCC) with tile-based thermal protection system (TPS) materials is the primary objective. Weight, complexity, coating impact damage, and repairability are among the problems that this tile technology development addresses. The following subtasks will be performed in this development effort: tile coating development; SIRCA tile development; robustness testing of tiles; tile repair development; tile operations/processing; tile leading edge configuration; and life cycle testing. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 95N28258
NASA-CR-198633
NAS 1.26:198633
SSD95D0239-PT-1 |
| 権利 | No Copyright |
