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Superfluid helium leak sealant studyTwenty-one leak specimens were fabricated in the ends of stainless steel and aluminum tubes. Eighteen of these tubes were coated with a copolymer material to seal the leak. The other three specimens were left uncoated and served as control specimens. All 21 tubes were cold shocked in liquid helium 50 times and then the leak rate was measured while the tubes were submerged in superfluid helium at 1.7 K. During the cold shocks two of the coated specimens were mechanically damaged and eliminated from the test program. Of the remaining 16 coated specimens one suffered a total coating failure and resulting high leak rate. Another three of the coated specimens suffered partial coating failures. The leak rates of the uncoated specimens were also measured and reported. The significance of various leak rates is discussed in view of the infrared astronomical satellite (IRAS) Dewar performance.
Document ID
19810007899
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vorreiter, J. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-81212
A-8233
Report Number: NASA-TM-81212
Report Number: A-8233
Accession Number
81N16415
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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