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Development of a Flexible Seal for a 60 psi Cryogenic Pressure BoxA cryogenic pressure box test facility has been designed and fabricated for use at NASA Langley Research Center (LaRC) to subject 5 ft x 6 ft curved panels to cryogenic temperatures and biaxial tensile loads. The cryogenic pressure box is capable of testing curved panels down to -423 F (20 K) with 54 psig maximum pressure. The key challenge in the design and fabrication of the pressure box was the development of a seal that could remain flexible at -423 F and contain 60 psi gaseous helium as the pressurization gas. A C-shaped seal was developed using a Gore-tex woven fabric. Mechanical testing of the fabric at room and elevated temperature, liquid nitrogen temperature, and liquid helium temperature demonstrated the strength and creep resistance of the material over the desired operating range. A small scale cryogenic pressure box was used to test prototype seals at cryogenic temperatures up to 60 psi. Preliminary tests indicated that excessive leakage was present through the seal. As a result, an aluminized mylar liner was placed inside the Gore-tex seal to reduce leakage through the seal. The final seal configuration resulted in minimal pressure loss during seal testing.
Document ID
19980197472
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Glass, David E.
(Analytical Services and Materials, Inc. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1998
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/CR-1998-207669
AS/M-LS05-02
NAS 1.26:207669
Report Number: NASA/CR-1998-207669
Report Number: AS/M-LS05-02
Report Number: NAS 1.26:207669
Funding Number(s)
CONTRACT_GRANT: G733056-J35
CONTRACT_GRANT: NAS1-96014
PROJECT: RTOP 242-33-01-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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