| タイトル | Development and Evaluation of High Temperature Gaskets for Hypersonic and Reentry Applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080003824 |
| 著者（英） | Shpargel, Tarah; Singh, Mrityunjay |
| 著者所属（英） | Ohio Aerospace Inst. |
| 発行日 | 2007-10-01 |
| 言語 | eng |
| 内容記述 | A wide variety of flexible gasket compositions were developed and tested at high temperatures. The gasket material system has high temperature capability. GRABER sealants were very effective in sealing machined ACC-4 composite surfaces. The gasket composition do not bond strongly with the ACC-4 substrate materials. The density of gasket materials can be tailored to show appropriate compressibility. |
| NASA分類 | Mechanical Engineering |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/564763 |
