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Testing Seam Concepts for Advanced Multilayer InsulationMultilayer insulation (MLI) is considered the state of the art insulation for cryogenic propellant tanks in the space environment. MLI traditionally consists of multiple layers of metalized films separated by low conductivity spacers. In order to better understand some of the details within MLI design and construction, GRC has been investigating the heat loads caused by multiple types of seams. To date testing has been completed with 20 layer and 50 layer blankets. Although a truly seamless blanket is not practical, a blanket lay-up where each individual layer was overlapped and tapped together was used as a baseline for the other seams tests. Other seams concepts tested included: an overlap where the complete blanket was overlapped on top of itself; a butt joint were the blankets were just trimmed and butted up against each other, and a staggered butt joint where the seam in the out layers is offset from the seam in the inner layers. Measured performance is based on a preliminary analysis of rod calibration tests conducted prior to the start of seams testing. Baseline performance for the 50 layer blanket showed a measured heat load of 0.46 Watts with a degradation to about 0.47 Watts in the seamed blankets. Baseline performance for the 20 layer blanket showed a measured heat load of 0.57 Watts. Heat loads for the seamed tests are still begin analyzed. So far analysis work has suggested the need for corrections due to heat loads from both the heater leads and the instrumentation wires. A careful re-examination of the calibration test results with these factors accounted for is also underway. This presentation will discuss the theory of seams in MLI, our test results to date, and the uncertainties in our measurements.
Document ID
20170008804
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Chato, D. J.
(NASA Glenn Research Center Cleveland, OH, United States)
Johnson, W. L.
(NASA Glenn Research Center Cleveland, OH United States)
Alberts, Samantha J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 14, 2017
Publication Date
July 5, 2017
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN44512
Report Number: GRC-E-DAA-TN44512
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 448887.04.03.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
multilayer insulation
cryogenic fluid management
Cryogenic propellants
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