| タイトル | Advanced Reusable Foam Cryogenic Insulation |
| 著者（英） | Sparks, L. L.; Mcauliffe, P. S.; Taylor, Allan H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1990-04-01 |
| 言語 | eng |
| 内容記述 | Lightweight, reusable cryogenic containers reduce costs of operation of advanced hypersonic airplanes and space launch vehicles. Specimens demonstrated in temperature range of negative 420 to positive 400 degrees F (negative 251 to positive 204 degrees C). Prototype reusable cryogenic foam insulation developed. Consists of two discrete layers of closed-cell polymethacrylimide foam of density 6.9 lb/ft to the 3rd power (111 kg/m to the 3rd power) bonded together with epoxy adhesive. Additionally reinforced with 0.003-in. (0.08-mm)-thick layer of fiberglass cloth. Wrapped with precut and preformed vapor-barrier cover. Such containers useful on Earth in laboratories, factories, and transportation systems. |
| NASA分類 | MATERIALS |
| レポートNO | 90B10166
LAR-14014 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/360945 |
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