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Thermally-Conductive Metallic Coatings and Applications for Heat Removal on In-Space Cryogenic Vehicles For large in-space cryogenic upper stages, substantial axial heat removal from a forward skirt by vapor-based heat interception may not be achieved by simple attachment methods unless sufficient thermal conductance from the skirt to the cooling fluid can be achieved. Preferable methods would allow for the addition of the cooling system to existing structure with minimal impact on the structure. Otherwise, significant modification to the basic structural design andor novel and complex attachment mechanisms with high effective thermal conductance are likely to be required. The approach being pursued by evolvable Cryogenics (eCryo) is to increase the thermal performance of a relatively simple attachment system by applying metallic or other thermally conductive material coatings to the mating surface area of the fluid channel where it is attached the skirt wall. The expectation of candidate materials is that the dramatic increase in conductivity of pure metals at temperatures close to liquid hydrogen vapor temperature will compensate for the reduced actual contact area typical of mechanical joints. Basic contact conductance data at low temperatures for candidate interface materials is required to enable the test approach. A test rig was designed at NASA Glenn Research Center to provide thermal contact resistance testing between small sample coupons coated with conductive material via electron beam evaporation, a low-temperature option that will not affect physical properties of base materials. Average coating thicknesses were 10 k. The test fixture was designed to mount directly to a cryocooler cold head within a vacuum test chamber. The purpose of this test was to determine qualitative contact conductance between various test samples. Results from this effort will be implemented in a sub-scale vapor-based heat interception test, where the applicability for increased heat removal on large structural skirts will be considered.
Document ID
20170008741
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Ameen, Lauren
(NASA Glenn Research Center Cleveland, OH United States)
Hervol, David
(Vantage Partners, LLC Cleveland, OH, United States)
Waters, Deborah
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 11, 2017
Publication Date
July 6, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN44304
Report Number: GRC-E-DAA-TN44304
Meeting Information
Meeting: Space Cryogenics Workshop
Location: Oak Brook, IL
Country: United States
Start Date: July 5, 2017
End Date: July 7, 2017
Sponsors: Cryogenic Society of America, Inc.
Funding Number(s)
WBS: WBS 448887.05.03.03
CONTRACT_GRANT: NNC12BA01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
small scale testing
Structural attachments
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