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Design, Development, and Testing of a Water Vapor Exchanger for Spacecraft Life Support SystemsThermal and environmental control systems for future exploration spacecraft must meet challenging requirements for efficient operation and conservation of resources. Maximizing the use of regenerative systems and conserving water are critical considerations. This paper describes the design, development, and testing of an innovative water vapor exchanger (WVX) that can minimize the amount of water absorbed in, and vented from, regenerative CO2 removal systems. Key design requirements for the WVX are high air flow capacity (suitable for a crew of six), very high water recovery, and very low pressure losses. We developed fabrication and assembly methods that enable high-efficiency mass transfer in a uniform and stable array of Nafion tubes. We also developed analysis and design methods to compute mass transfer and pressure losses. We built and tested subscale units sized for flow rates of 2 and 5 cu ft/min (3.4–8.5 cu m/hr). Durability testing demonstrated that a stable core geometry was sustained over many humid/dry cycles. Pressure losses were very low (less than 0.5 in. H2O (125 Pa) total) and met requirements at prototypical flow rates. We measured water recovery efficiency across a range of flow rates and humidity levels that simulate the range of possible cabin conditions. We measured water recovery efficiencies in the range of 80 to 90%, with the best efficiency at lower flow rates and higher cabin humidity levels. We compared performance of the WVX with similar units built using an unstructured Nafion tube bundle. The WVX achieves higher water recovery efficiency with nearly an order of magnitude lower pressure drop than unstructured tube bundles. These results show that the WVX provides uniform flow through flow channels for both the humid and dry streams and can meet requirements for service on future exploration spacecraft. The WVX technology will be best suited for long-duration exploration vehicles that require regenerative CO2 removal systems while needing to conserve water.
Document ID
20160014040
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Izenson, Michael G.
(Creare, Inc. Hanover, NH, United States)
Micka, Daniel J.
(Creare, Inc. Hanover, NH, United States)
Chepko, Ariane B.
(Creare, Inc. Hanover, NH, United States)
Rule, Kyle C.
(Creare, Inc. Hanover, NH, United States)
Anderson, Molly S.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
December 1, 2016
Publication Date
July 10, 2016
Subject Category
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-36617
ICES-2016-231
Report Number: JSC-CN-36617
Report Number: ICES-2016-231
Meeting Information
Meeting: International Conference on Environmental Systems (ICES) 2016
Location: Vienna
Country: Austria
Start Date: July 10, 2016
End Date: July 14, 2016
Sponsors: International Conference On Environmental Systems, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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