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NASA NTRS · 19910021922

Composite Flexible Blanket Insulation

Abstract

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.

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BibTeXRIS

Kourtides, Demetrius A., Pitts, William C., Goldstein, Howard E., Sawko, Paul M.. 1991-08-13. Composite Flexible Blanket Insulation. https://ntrs.nasa.gov/citations/19910021922

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