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Variable Density Multilayer Insulation for Cryogenic StorageTwo analytical models for a foam/Variable Density Multi-Layer Insulation (VD-MLI) system performance are discussed. Both models are one-dimensional and contain three heat transfer mechanisms, namely conduction through the spacer material, radiation between the shields, and conduction through the gas. One model is based on the methodology developed by McIntosh while the other model is based on the Lockheed semi-empirical approach. All models input variables are based on the Multi-purpose Hydrogen Test Bed (MHTB) geometry and available values for material properties and empirical solid conduction coefficient. Heat flux predictions are in good agreement with the MHTB data, The heat flux predictions are presented for the foam/MLI combinations with 30, 45, 60, and 75 MLI layers
Document ID
20000092076
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hedayat, A.
(Sverdrup Technology, Inc. Huntsville, AL United States)
Brown, T. M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Hastings, L. J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Martin, J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: 36th Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: July 17, 2000
End Date: July 19, 2000
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
CONTRACT_GRANT: NAS8-40836
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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