| タイトル | NASA Langley Research Center National Aero-Space Plane Mission simulation profile sets |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900019225 |
| 著者（英） | Bresina, John J.; Vaughn, Wallace L.; Ohlhorst, Craig W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1990-10-01 |
| 言語 | eng |
| 内容記述 | To provide information on the potential for long life service of oxidation resistant carbon-carbon (ORCC) materials in the National Aero-Space Plane (NASP) airframe environment, NASP ascent, entry, and cruise trajectories were analytically flown. Temperature and pressure profiles were generated for 20 vehicle locations. Orbital (ascent and entry) and cruise profile sets from four locations are presented along with the humidity exposure and testing sequences that are being used to evaluate ORCC materials. The four profiles show peak temperatures during the ascent leg of an orbital mission of 2800, 2500, 2000, and 1700 F. These profiles bracket conditions where carbon-carbon might be used on the NASP vehicle. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 90N28541
NASA-TM-102670
NAS 1.15:102670 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/136354 |
