| タイトル | Thermal Analysis of the X-38 Aft Fin During Re-Entry |
| 著者（英） | Hong, Andrew E. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1999-11-01 |
| 言語 | eng |
| 内容記述 | This document contains the details of the thermal analysis of the X-38 aft fin during re-entry. This analysis was performed in order to calculate temperature response of the aft fin components. This would be provided as input to a structural analysis and would also define the operating environment for the electromechanical actuator (EMA). The calculated structural temperature response would verify the performance of the thermal protection system (TPS). The geometric representation of the aft fin was derived from an I-DEAS finite element model that was used for structural analysis. The thermal mass network model was derived from the geometric representation. |
| NASA分類 | Aerodynamics |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/539296 |
