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Development of a Compact, Efficient Cooling Pump for Space Suit Life Support SystemsA compact, low-power electrochemically-driven fluid cooling pump is currently being developed by Lynntech, Inc. With no electric motor and minimal lightweight components, the pump is significantly lighter than conventional rotodynamic and displacement pumps. Reliability and robustness is achieved with the absence of rotating or moving components (apart from the bellows). By employing sulfonated polystyrene-based proton exchange membranes, rather than conventional Nafion membranes, a significant reduction in the actuator power consumption was demonstrated. Lynntech also demonstrated that these membranes possess the necessary mechanical strength, durability, and temperature range for long life space operation. The preliminary design for a Phase II prototype pump compares very favorably to the fluid cooling pumps currently used in space suit primary life support systems (PLSSs). Characteristics of the electrochemically-driven pump are described and the benefits of the technology as a replacement for electric motor pumps in mechanically pumped single-phase fluid loops is discussed.
Document ID
20090020497
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
van Boeyen, Roger
(Lynntech College Station, TX, United States)
Reeh, Jonathan
(Lynntech College Station, TX, United States)
Trevino, Luis
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2009
Subject Category
Man/System Technology And Life Support
Report/Patent Number
09ICES-0305
JSC-CN-18104
Meeting Information
Meeting: 39th International Conference on Environmental Systems
Location: Savannah, GA
Country: United States
Start Date: July 12, 2009
End Date: July 16, 2009
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
OTHER: 903 184.04k.02.02.02
Distribution Limits
Public
Copyright
Other

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