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Metabolic Heat Regenerated Temperature Swing Adsorption for CO2 and Heat Removal/Rejection in a Martian PLSSTwo of the fundamental problems facing the development of a Portable Life Support System (PLSS) for use on Mars, are (i) heat rejection (because traditional technologies use sublimation of water, which wastes a scarce resource and contaminates the premises), and (ii) rejection of carbon dioxide (CO2) in an environment with a CO2 partial pressure (ppCO2) of 0.4-0.9 kPa. Patent-pending Metabolic heat regenerated Temperature Swing Adsorption (MTSA) technology is being developed to address both these challenges. The technology utilizes an adsorbent that when cooled with liquid CO2 to near sublimation temperatures (~195K) removes metabolically-produced CO2 in the ventilation loop. Once fully loaded, the adsorbent is then warmed externally by the ventilation loop (~300K), rejecting the captured CO2 to Mars ambient. Two beds are used to provide a continuous cycle of CO2 removal/rejection as well as facilitate heat exchange out of the ventilation loop. Any cryogenic fluid can be used in the application; however, since CO2 is readily available on Mars and can be easily produced and stored on the Martian surface, the solution is rather elegant and less complicated when employing liquid CO2. As some metabolic heat will need to be rejected anyway, finding a practical use for metabolic heat is also an overall benefit to the PLSS. To investigate the feasibility of the technology, a series of experiments were conducted which lead to the selection and partial characterization of an appropriate adsorbent. The Molsiv Adsorbents 13X 8x12 (also known as NaX zeolite) successfully removed CO2 from a simulated ventilation loop at the prescribed temperature swing anticipated during PLSS operating conditions on Mars using a cryogenic fluid. Thermal conductivity of the adsorbent was also measured to eventually aid in a demonstrator design of the technology. These results provide no show stoppers to the development of MTSA technology and allow its development to focus on other design challenges as listed in the conclusions section of this paper.
Document ID
20070016701
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Iacomini, Christine
(Paragon Space Development Corp. AZ, United States)
Powers, Aaron
(Paragon Space Development Corp. AZ, United States)
Bower, Chad
(Paragon Space Development Corp. AZ, United States)
Straub-Lopez, Kathrine
(Paragon Space Development Corp. AZ, United States)
Anderson, Grant
(Paragon Space Development Corp. AZ, United States)
MacCallum, Taber
(Paragon Space Development Corp. AZ, United States)
Paul, Heather L.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
July 12, 2007
Subject Category
Man/System Technology And Life Support
Report/Patent Number
07ICES-243
Report Number: 07ICES-243
Meeting Information
Meeting: ICES
Location: Chicago, IL
Country: United States
Start Date: July 9, 2007
End Date: July 12, 2007
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
WBS: WBS 731384.06.04.01.05.10
CONTRACT_GRANT: NNJ06HA98C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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