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Thermal Performance of Cryogenic Piping Multilayer Insulation in Actual Field InstallationsA standardized way of comparing the thermal performance of different pipelines in different sizes is needed. Vendor data for vacuum-insulated piping are typically given in heat leak rate per unit length (W/m) for a specific diameter pipeline. An overall k-value for actual field installations (k(sub oafi)) is therefore proposed as a more generalized measure for thermal performance comparison and design calculation. The k(sub oafi) provides a direct correspondence to the k-values reported for insulation materials and illustrates the large difference between ideal multilayer insulation (MLI) and actual MLI performance. In this experimental research study, a section of insulated piping was tested under cryogenic vacuum conditions, including simulated spacers and bending. Several different insulation systems were tested using a 1-meter-long cylindrical cryostat test apparatus. The simulated spacers tests showed significant degradation in the thermal performance of a given insulation system. An 18-meter-long pipeline test apparatus is now in operation at the Cryogenics Test Laboratory, NASA Kennedy Space Center, for conducting liquid nitrogen thermal performance tests.
Document ID
20020039045
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Fesmire, J.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Augustnynowicz, S.
(DYNACS Engineering Co., Inc. Cocoa Beach, FL United States)
Thompson, K.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Cryogenics 2002
Location: Prague
Country: Czechoslovakia
Start Date: April 15, 2002
End Date: April 19, 2002
Funding Number(s)
CONTRACT_GRANT: NAS10-98001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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