| タイトル | Seal Sample Fixtures |
| 本文（外部サイト） | http://hdl.handle.net/2060/19990010680 |
| 著者（英） | Hadaway, James B.; White, Edwin |
| 著者所属（英） | Alabama Univ. |
| 発行日 | 1997-03-01 |
| 言語 | eng |
| 内容記述 | The development of the International Space Station is critically dependent upon development and testing of materials that will require exposure to the space environment. The seals between the modules are one of the more important examples. The choice of seals depends upon the seal materials' susceptibility to atomic oxygen, UV radiation, and the combined external space environment. Also, the choice of thermal control materials depends on their susceptibility to the space environment. The Space Environmental Branch at MSFC developed a flight experiment to provide information on the effects of the space environment on seal and thermal control materials. The experiment, called the Passive Optical Sample Array (POSA), involved exposing several different material samples to the atomic oxygen, UV radiation, and combined effects of the space environment. The POSA experiment is currently flying on the Russian Mir space station. It was necessary during the assembly of POSA to develop an understanding of available fabrication and metrology techniques in order to develop several monitoring systems for the experiment. The report briefly describes the tasks and the work performed in preparing the samples for the POSA experiment. |
| NASA分類 | Mechanical Engineering |
| レポートNO | NASA-CR-202796
UAH-4
NAS 1.26:202796 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/97005 |
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