| タイトル | Wind tunnel tests of space shuttle solid rocket booster insulation material in the aerothermal tunnel c |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830011537 |
| 著者（英） | Hartman, A. S.; Nutt, K. W. |
| 著者所属（英） | Calspan Field Services, Inc. |
| 発行日 | 1982-11-01 |
| 言語 | eng |
| 内容記述 | Wind tunnel tests of the space shuttle Solid Rocket Booster Insulation were conducted in the von Karman Gas Dynamics Facility Tunnel C. For these tests, Tunnel C was run at Mach 4 with a total temperature of 1100-1440 and a total pressure of 100 psia. Cold wall heating rates were changed by varying the test article support wedge angle. Selected results are presented to illustrate the test techniques and typical data obtained. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 83N19808
AEDC-TSR-82-V38 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163225 |
