| タイトル | Reusable cryogenic foam insulation for advanced aerospace vehicles |
| 著者（英） | Taylor, Allan H.; Dube, William P.; Sparks, Larry L.; Mcauliffe, Patrick S. |
| 著者所属（英） | National Inst. of Standards and Technology; NASA Langley Research Center; Lockheed Aeronautical Systems Co. |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | Future high-speed aircraft and aerospace vehicles using cryogenic propellants will require an advanced reusable insulation system for the propellant tank structure. This cryogenic insulation system must be lightweight, structurally and thermally efficient, and capable of multiple reuse without cracking or degraded performance. This paper presents recent progress in the development of a reusable cryogenic foam insulation system having a maximum service temperature of 400 F. The system consists of preshaped, precut blocks of rigid polymethacrylimide foam insulation, wrapped with a high-temperature Kapton and aluminum foil vapor barrier which is adhesively bonded to the propellant tank wall. |
| NASA分類 | NONMETALLIC MATERIALS |
| レポートNO | 91A21524
AIAA PAPER 91-0542 |
| 権利 | Copyright |
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