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Two-Phase Cryogenic Heat Exchanger for the Thermodynamic Vent SystemA two-phase cryogenic heat exchanger for a thermodynamic vent system was designed and analyzed, and the predicted performance was compared with test results. A method for determining the required size of the Joule-Thomson device was also developed. Numerous sensitivity studies were performed to show that the design was robust and possessed a comfortable capacity margin. The comparison with the test results showed very similar heat extraction performance for similar inlet conditions. It was also shown that estimates for Joule- Thomson device flow rates and exit quality can vary significantly and these need to be accommodated for with a robust system design.
Document ID
20110020836
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Christie, Robert J.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
E-17903
NASA/TM-2011-217220
Report Number: E-17903
Report Number: NASA/TM-2011-217220
Funding Number(s)
WBS: WBS 095240.04.13.01.14.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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