| タイトル | Reusable High-Temperature/Cryogenic Foam-Insulation System |
| 著者（英） | Taylor, Allan H.; Mcauliffe, Patrick; Jackson, L. Robert; Davis, Randall C. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-05-01 |
| 言語 | eng |
| 内容記述 | Flightweight insulation withstands wide temperture cycling. Reusable insulation system for cryogenic containment vessels withstands repeated exposures to thermal environments that span ranges from cryogenic-fluid temperature {-425oF (-254oC)} to maximum use temperature of containment-tank material {+400oF (+204oC)}. System designed for use with high-speed flight vehicles. |
| NASA分類 | MATERIALS |
| レポートNO | 87B10227
LAR-13506 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/382434 |
