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Improved Thermal-Insulation Systems for Low TemperaturesImproved thermal-insulation materials and structures and the techniques for manufacturing them are undergoing development for use in low-temperature applications. Examples of low-temperature equipment for which these thermal insulation systems could provide improved energy efficiency include storage tanks for cryogens, superconducting electric-power-transmission equipment, containers for transport of food and other perishable commodities, and cold boxes for low-temperature industrial processes. These systems could also be used to insulate piping used to transfer cryogens and other fluids, such as liquefied natural gas, refrigerants, chilled water, crude oil, or low-pressure steam. The present thermal-insulation systems are layer composites based partly on the older class of thermal-insulation systems denoted generally as multilayer insulation (MLI). A typical MLI structure includes an evacuated jacket, within which many layers of radiation shields are stacked or wrapped close together. Low-thermal-conductivity spacers are typically placed between the reflection layers to keep them from touching. MLI can work very well when a high vacuum level (less than 10(exp-4) torr) is maintained and utmost care is taken during installation, but its thermal performance deteriorates sharply as the pressure in the evacuated space rises into the soft vacuum range [pressures greater than 0.1 torr (greater than 13 Pa)]. In addition, the thermal performance of MLI is extremely sensitive to mechanical compression and edge effects and can easily decrease from one to two orders of magnitude from its ideal value even when the MLI is kept under high vacuum condition. The present thermal-insulation systems are designed to perform well under soft vacuum level, in particular the range of 1 to 10 torr. They are also designed with larger interlayer spacings to reduce vulnerability to compression (and consequent heat leak) caused by installation and use. The superiority of these systems is the synergistic effect of improvements in materials, design, and manufacture.
Document ID
20110023905
Acquisition Source
Kennedy Space Center
Document Type
Other - NASA Tech Brief
Authors
Fesmire, James E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Augustynowicz, Stanislaw D.
(DYNACS Engineering Co., Inc. Cocoa Beach, FL, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2003
Publication Information
Publication: NASA Tech Briefs, September 2003
Subject Category
Man/System Technology And Life Support
Report/Patent Number
KSC-12092
Distribution Limits
Public
Copyright
Public Use Permitted.
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