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Advanced Reusable Foam Cryogenic InsulationLightweight, reusable cryogenic containers reduce costs of operation of advanced hypersonic airplanes and space launch vehicles. Specimens demonstrated in temperature range of negative 420 to positive 400 degrees F (negative 251 to positive 204 degrees C). Prototype reusable cryogenic foam insulation developed. Consists of two discrete layers of closed-cell polymethacrylimide foam of density 6.9 lb/ft to the 3rd power (111 kg/m to the 3rd power) bonded together with epoxy adhesive. Additionally reinforced with 0.003-in. (0.08-mm)-thick layer of fiberglass cloth. Wrapped with precut and preformed vapor-barrier cover. Such containers useful on Earth in laboratories, factories, and transportation systems.
Document ID
19900000166
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Taylor, Allan H.
(NASA Langley Research Center, Hampton, VA.)
Mcauliffe, P. S.
(Lockheed-California Co.)
Sparks, L. L.
(National Bureau of Standards)
Date Acquired
August 14, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 4
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LAR-14014
Accession Number
90B10166
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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