| タイトル | A study of the effect on a typical orbiter payload thermal environment resulting from specular reflections from the forward orbiter radiators |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800012924 |
| 著者（英） | Humphries, R.; Littles, J. W.; Turner, L. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1979-03-01 |
| 言語 | eng |
| 内容記述 | The orbiter radiator external coating is highly specular silverized Teflon. Solar energy specularly reflected from these radiators on a typical payload which, when deployed, extends above the payload bay envelope was studied. The flux levels are compared assuming both diffuse and specular radiators. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 80N21409
NASA-TM-78270 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/172886 |
