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Lightweight Ceramic InsulationFiber burnout process yields low densities. Low density attained by process of sacrificial burnout. Graphite or carbon fibers mixed into slurry of silica, alumina, and boron-compound fibers in amounts ranging from 25 to 75 percent of total fiber content by weight. Mixture formed into blocks and dried. Blocks placed in kiln and heated to 1,600 degrees F(870 degrees C) for several hours. Graphite or carbon fibers slowly oxidize away, leaving voids and reducing block density. Finally, blocks heated to 2,350 degrees F (1,290 degrees C) for 90 minutes to bond remaining ceramic fibers together. Developed for use on Space Shuttle and other spacecraft, rigid insulation machined to requisite shape and bonded in place.
Document ID
19860000223
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wheeler, W. H.
(Lockheed Missiles & Space Co., Inc.)
Creedon, J. F.
(Lockheed Missiles & Space Co., Inc.)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 3
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
MSC-20831
Accession Number
86B10223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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