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Freezable Radiator Model Correlation and Full Scale DesignFreezable radiators offer an attractive solution to the issue of thermal control system scalability. As thermal environments change, a freezable radiator will effectively scale the total heat rejection it is capable of as a function of the thermal environment and flow rate through the radiator. Scalable thermal control systems are a critical technology for spacecraft that will endure missions with widely varying thermal requirements. These changing requirements are a result of the space craft s surroundings and because of different thermal loads during different mission phases. However, freezing and thawing (recovering) a radiator is a process that has historically proven very difficult to predict through modeling, resulting in highly inaccurate predictions of recovery time. This paper summarizes efforts made to correlate a Thermal Desktop (TM) model with empirical testing data from two test articles. A 50-50 mixture of DowFrost HD and water is used as the working fluid. Efforts to scale this model to a full scale design, as well as efforts to characterize various thermal control fluids at low temperatures are also discussed.
Document ID
20110001563
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Lillibridge, Sean T.
(NASA Johnson Space Center Houston, TX, United States)
Navarro, Moses
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-22090
Report Number: JSC-CN-22090
Meeting Information
Meeting: International Conference on Environmental Systems (ICES) conference
Location: Portland, OR
Country: United States
Start Date: July 17, 2011
End Date: July 21, 2011
Distribution Limits
Public
Copyright
Public Use Permitted.
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