| タイトル | Investigation of configuration effects on entry heating distributions at Mach no. equals 8.0 (OH41A) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740002691 |
| 著者（英） | Gorowitz, H.; White, R.; D'Errico, A. |
| 著者所属（英） | Chrysler Corp. |
| 発行日 | 1973-09-01 |
| 言語 | eng |
| 内容記述 | The results are presented of aerodynamic heating investigations conducted on 0.006 scale models of three Rockwell International Space Shuttle Vehicles (SSV) orbiter configurations in the Mach 8 variable density tunnel. It was established that lower surface modifications to one of these configurations (Model SS-H-00326-4) would alleviate premature transition. Re-entry data were acquired on these models at angles of attack from 30 to 40 degrees for nominal Reynolds numbers per foot of 1.0, 3.0, 6.0 and 8.0 million utilizing the phase change paint technique. A total of 17 orbiter heating runs and 3 orbiter oil flow runs were completed. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74N10804
DMS-DR-2076
NASA-CR-128785 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/196922 |
