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タイトルComposite Flexible Blanket Insulation
本文(外部サイト)http://hdl.handle.net/2060/19910021922
著者(英)Sawko, Paul M.; Kourtides, Demetrius A.; Pitts, William C.; Goldstein, Howard E.
著者所属(英)NASA Pasadena Office|Jet Propulsion Lab., California Inst. of Tech.|Eloret Corp.
発行日1991-08-13
言語eng
内容記述Composite flexible multilayer insulation systems (MLI) were evaluated for thermal performance and compared with the currently used fibrous silica (baseline) insulation system. The systems described are multilayer insulations consisting of alternating layers of metal foil and scrim ceramic cloth or vacuum metallized polymeric films quilted together using ceramic thread. A silicon carbide thread for use in the quilting and the method of making it are also described. These systems are useful in providing lightweight insulation for a variety of uses, particularly on the surface of aerospace vehicles subject to very high temperatures during flight.
NASA分類COMPOSITE MATERIALS
レポートNO91N31236
権利No Copyright


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