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Composite multilayer insulations for thermal protection of aerospace vehiclesComposite flexible multilayer insulation systems (MLI), consisting of alternating layers of metal foil and scrim cloth or insulation quilted together using ceramic thread, were evaluated for thermal performance and compared with a silica fibrous (baseline) insulation system. The systems studied included: (1) alternating layers of aluminoborosilicate (ABS) scrim cloth and stainless steel foil, with silica, ABS, or alumina insulation; (2) alternating layers of scrim cloth and aluminum foil, with silica or ABS insulation; (3) alternating layers of alumininum foil and silica or ABS insulation; and (4) alternating layers of aluminum-coated polyimide placed on the bottom of the silica insulation. The MLIs containing aluminum were the most efficient, measuring as little as half the backface temperature increase of the baseline system.
Document ID
19900000867
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kourtides, D. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Pitts, W. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1989
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-101071
A-89035
NAS 1.15:101071
Report Number: NASA-TM-101071
Report Number: A-89035
Report Number: NAS 1.15:101071
Meeting Information
Meeting: Composites in Manufacturing 8 Exposition and Conference, Society of Manufacturing Engineers
Location: Anaheim, CA
Country: United States
Start Date: January 9, 1989
End Date: January 12, 1989
Accession Number
90N10183
Funding Number(s)
PROJECT: RTOP 506-43-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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