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Study of thermal insulation for airborne liquid hydrogen fuel tanksA concept for a fail-safe thermal protection system was developed. From screening tests, approximately 30 foams, adhesives, and reinforcing fibers using 0.3-meter square liquid nitrogen cold plate, CPR 452 and Stafoam AA1602, both reinforced with 10 percent by weight of 1/16 inch milled OCF Style 701 Fiberglas, were selected for further tests. Cyclic tests with these materials in 2-inch thicknesses bonded on a 0.6-meter square cold plate with Crest 7410 adhesive systems, were successful. Zero permeability gas barriers were identified and found to be compatible with the insulating concept.
Document ID
19780024353
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ruccia, F. E.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Lindstrom, R. S.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Lucas, R. M.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Engineering (General)
Report/Patent Number
NASA-CR-158920
Report Number: NASA-CR-158920
Accession Number
78N32296
Funding Number(s)
CONTRACT_GRANT: NAS1-14157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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