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Reusable High-Temperature/Cryogenic Foam-Insulation SystemFlightweight insulation withstands wide temperture cycling. Reusable insulation system for cryogenic containment vessels withstands repeated exposures to thermal environments that span ranges from cryogenic-fluid temperature {-425oF (-254oC)} to maximum use temperature of containment-tank material {+400oF (+204oC)}. System designed for use with high-speed flight vehicles.
Document ID
19870000227
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Davis, Randall C. (NASA Langley Research Center, Hampton, Va.)
Taylor, Allan H. (NASA Langley Research Center, Hampton, Va.)
Jackson, L. Robert (NASA Langley Research Center, Hampton, Va.)
Mcauliffe, Patrick (Lockheed Aircraft Co.)
Date Acquired
August 13, 2013
Publication Date
May 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 5
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LAR-13506
ISSN: 0145-319X
Report Number: LAR-13506
Accession Number
87B10227
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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