| タイトル | Users guide: Steady-state aerodynamic-loads program for shuttle TPS tiles |
| 本文（外部サイト） | http://hdl.handle.net/2060/19860017934 |
| 著者（英） | Kerr, P. A.; Petley, D. H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1984-07-01 |
| 言語 | eng |
| 内容記述 | A user's guide for the computer program that calculates the steady-state aerodynamic loads on the Shuttle thermal-protection tiles is presented. The main element in the program is the MITAS-II, Martin Marietta Interactive Thermal Analysis System. The MITAS-II is used to calculate the mass flow in a nine-tile model designed to simulate conditions duing a Shuttle flight. The procedures used to execute the program using the MITAS-II software are described. A list of the necessry software and data files along with a brief description of their functions is given. The format of the data file containing the surface pressure data is specified. The interpolation techniques used to calculate the pressure profile over the tile matrix are briefly described. In addition, the output from a sample run is explained. The actual output and the procedure file used to execute the program at NASA Langley Research Center on a CDC CYBER-175 are provided in the appendices. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 86N27406
NASA-TM-85724
NAS 1.15:85724 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/153907 |
