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Effects of Surfactant Contamination on the Next Generation Gas Trap for the ISS Internal Thermal Control SystemThe current dual-membrane gas trap is designed to remove non-condensed gas bubbles from the Internal Thermal Control System (ITCS) coolant on board the International Space Station (ISS). To date it has successfully served its purpose of preventing gas bubbles from causing depriming, overspeed, and shutdown of the ITCS pump. However, contamination in the ITCS coolant has adversely affected the gas venting rate and lifetime of the gas trap, warranting a development effort for a next-generation gas trap. Previous testing has shown that a hydrophobic-only design is capable of performing even better than the current dual-membrane design for both steady-state gas removal and gas slug removal in clean deionized water. This paper presents results of testing to evaluate the effects of surfactant contamination on the steady-state performance of the hydrophobic-only design.
Document ID
20040085978
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Leimkuehler, Thomas O.
(Honeywell, Inc. United States)
Lukens, Clark
(Honeywell, Inc. United States)
Reeves, Daniel R.
(Boeing Co. United States)
Holt, James M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SAE-04ICES-203
Meeting Information
Meeting: 2004 International Conference on Environmental Systems 34th Annual Meeting
Location: Colorado Springs, CO
Country: United States
Start Date: July 19, 2004
End Date: July 22, 2004
Sponsors: Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Other

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