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Shuttle active thermal control system development testing. Volume 7: Improved radiator coating adhesive testsSilver/Teflon thermal control coatings have been tested on a modular radiator system projected for use on the space shuttle. Seven candidate adhesives have been evaluated in a thermal vacuum test on radiator panels similar to the anticipated flight hardware configuration. Several classes of adhesives based on polyester, silicone, and urethane resin systems were tested. These included contact adhesives, heat cured adhesives, heat and pressure cured adhesives, pressure sensitive adhesives, and two part paint on or spray on adhesives. The coatings attached with four of the adhesives, two silicones and two urethanes, had no changes develop during the thermal vacuum test. The two silicone adhesives, both of which were applied to the silver/Teflon as transfer laminates to form a tape, offered the most promise based on application process and thermal performance. Each of the successful silicone adhesives required a heat and pressure cure to adhere during the cryogenic temperature excursion of the thermal-vacuum test.
Document ID
19740026234
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reed, M. W.
(LTV Aerospace Corp. Dallas, TX, United States)
Date Acquired
September 3, 2013
Publication Date
November 16, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-140274
TI69-28-VOL-7
Report Number: NASA-CR-140274
Report Number: TI69-28-VOL-7
Accession Number
74N34347
Funding Number(s)
CONTRACT_GRANT: NAS9-10534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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