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SRB attach ring phenolic TPS fishtail seal evaluation testsThe SRB attach ring is thermally protected with layered phenolic cloth fairings that are fastened to the ring. The gap between the fairings and the motor case is closed off with a rubber seal of a fishtail cross sectional shape bonded to the phenolic. On both the STS-1 and STS-2 flights this gap was discovered to vary anywhere from an intended gap of 0.375 in. to an actual measured gap of 0.60 in. due to tolerances. Tests were conducted with and without a 0.25 in. thick cork shim placed under the seal with a 0.60 in. gap under the phenolic TPS to determine and compare the performance of the seal in the two different configurations. To alleviate the difficult and costly procedure of installing the cork shim under the seal, especially after phenolic TPS mounting on the attach ring, large fishtail seals of idential Elder gray silicon material and two different hardnesses were tested. A similar matrix of tests was conducted with this new large fishtail seal, and seals with both type hardnesses performed well regardless of whether or not the seal was bonded in the phenolic at the front of the seal groove. Similar results had been obtained with the original small fishtail seal which performed adequately with the 0.25 in. cork shim under it.
Document ID
19850027094
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Karu, Z. S.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1982
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:170887
NASA-CR-170887
LMSC-HREC-TM-D784769
Report Number: NAS 1.26:170887
Report Number: NASA-CR-170887
Report Number: LMSC-HREC-TM-D784769
Accession Number
85N35407
Funding Number(s)
CONTRACT_GRANT: NAS8-32982
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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