| タイトル | Options for improving rigidized ceramic heatshields |
| 著者（英） | Leiser, D. B.; Stewart, D. A.; Smith, M. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1985-08-01 |
| 言語 | eng |
| 内容記述 | Studies regarding capabilities, tensile strength, and dimensional stability of fibrous ceramics, used in current thermal protection systems and those required for future NASA advanced transfer vehicles, are presented. It is shown that the use of smaller diameter (2-4 micron) aluminoborosilicate fibers (instead of conventional 11-micron size) in the FRCI composites improves the homogeneity and tensile strength of high-silica composite. Substitution of the smaller aluminoborosilicate fibers by 2-4-micron alumina fibers in the AETB composites improves the dimensional stability, at the expense of a substantial increase in the thermal expansion coefficient, with a potential decrease in tensile strength. |
| NASA分類 | COMPOSITE MATERIALS |
| レポートNO | 86A15219 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/387644 |
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