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Performance of Water Recirculation Loop Maintentance Components for the Advanced Spacesuit Water Membrane EvaporatorWater loop maintenance components to maintain the water quality of the Advanced Spacesuit Water Membrane Evaporation (SWME) water recirculation loop have undergone a comparative performance evaluation with a second SWME water recirculation loop with no water quality maintenance. Results show the benefits of periodic water maintenance. The SWME is a heat rejection device under development at the NASA Johnson Space Center to perform thermal control for advanced spacesuits. One advantage to this technology is the potential for a significantly greater degree of tolerance to contamination when compared to the existing Sublimator technology. The driver for the evaluation of water recirculation maintenance components was to further enhance this advantage through the leveraging of fluid loop management lessonslearned from the International Space Station (ISS). A bed design that was developed for a UTAS military application, and considered for a potential ISS application with the Urine Processor Assembly, provided a low pressure drop means for water maintenance in a recirculation loop. The bed design is coupled with high capacity ion exchange resins, organic adsorbents, and a cyclic methodology developed for the Extravehicular Mobility Unit (EMU) Transport Water loop. The maintenance cycle included the use of a biocide delivery component developed for ISS to introduce a biocide in a microgravity-compatible manner for the Internal Active Thermal Control System (IATCS). The leveraging of these water maintenance technologies to the SWME recirculation loop is a unique demonstration of applying the valuable lessons learned on the ISS to the next generation of manned spaceflight Environmental Control and Life Support System (ECLSS) hardware.
Document ID
20140011730
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Rector, Tony
(United Technologies Aerospace Systems Windsor Locks, CT, United States)
Peyton, Barbara
(United Technologies Aerospace Systems Windsor Locks, CT, United States)
Steele, John W.
(United Technologies Aerospace Systems Windsor Locks, CT, United States)
Bue, Grant C.
(NASA Johnson Space Center Houston, TX, United States)
Campbell, Colin
(NASA Johnson Space Center Houston, TX, United States)
Makinen, Janice
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
September 16, 2014
Publication Date
July 13, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-30275
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Tuscon, AZ
Country: United States
Start Date: July 13, 2014
End Date: July 17, 2014
Sponsors: Texas Tech Univ.
Funding Number(s)
CONTRACT_GRANT: NNJ12HE86D
OTHER: GS-10F-0439X
Distribution Limits
Public
Copyright
Public Use Permitted.
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