| タイトル | Thermal response of integral multicomponent composites to a high-energy aerothermodynamic heating environment with surface temperature to 1800 K |
| 著者（英） | Leiser, Daniel B.; Stewart, David A. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1987-08-01 |
| 言語 | eng |
| 内容記述 | Laminated composite insulations developed for potential use on advanced spacecraft operating between GEO and LEO were tested in an aerothermodynamic environment simulating an AOTV aerobraking maneuver (altitude 82.3 km and velocity = 9.0 km/s). Comparisons are discussed between these data and predictions of in-depth temperature response using dynamical thermal conductivity values to 2000 K. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 88A12591 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/374503 |
