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Reliable and Efficient Electrochemical Recovery of O2 from Metabolic CO2 at the International Space Station (ISS)Maximum O2 recovery from metabolic carbon dioxide (CO2) is desired for future long-duration missions beyond Low Earth Orbit (LEO). The O2 recovery for the Environmental Control and Life Support System (ECLSS) at the International Space Station (ISS), presently limited to 50% (Sabatier), must be highly reliable and efficient and recover a minimum of 75% oxygen (O2) from metabolic CO2. An alternative technology development effort currently underway at NASA Marshall Space Flight Center (MSFC) via a Microfluidic Electrochemical Reactor (MFECR) approach has the potential to increase O2 recovery significantly and reduce the complexity of the ECLSS O2 recovery at the ISS as it would replace three pieces, the CO2 Reduction Assembly (CRA) (Sabatier reactor), the Oxygen Generation Assembly (OGA), and the Plasma Pyrolysis Assembly (PPA). The MFECR's electrochemical process generates ethylene (C2H4) and carbon moxide (CO) instead of methane (CH4) (Sabatier) as a byproduct, eliminating the need for further dehydrogenation through the PPA. As in the OGA, the MFECR's electrochemical process generates O2 and hydrogen (H2) from the water electrolysis process. MSFC and the University of Texas in Arlington (UTA) have jointly designed and fabricated an MFECR's single cell that operates at ambient conditions and utilizes a proprietary catalysis highly selective on reducing CO2 to C2H4 and CO at the cathode. This MFECR's single cell consists of gas diffusion layers at the cathode and anode for respective intake of CO2 and output of O2 from the catalytic layer. This approach is expected to substantially improve the ISS ECLSS sustainability and reduce power and weight requirements as the MFECR would replace three units currently installed in the ISS. In this paper, the authors discuss the outcome of preliminary tests, the current development, and the evaluation efforts on different alternatives for the cathode and the anode configurations, the setup of the MFECR at an engineering development unit (EDU) scale, and the O2 recovery performance, and evaluation efforts on different alternatives on not only the configuration and setup of the MFECR at an Engineering Design Unit (EDU) scale but also the selection of component materials.
Document ID
20240002161
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Jesus A Dominguez ORCID
(Jacobs (United States) Dallas, Texas, United States)
Lorlyn Reidy
(Marshall Space Flight Center Redstone Arsenal, United States)
Mononita Nur
(Marshall Space Flight Center Redstone Arsenal, United States)
Kagen Crawford
(Marshall Space Flight Center Redstone Arsenal, United States)
Brittany Brown
(Marshall Space Flight Center Redstone Arsenal, United States)
Brian Dennis ORCID
(The University of Texas at Arlington Arlington, Texas, United States)
Wilaiwan Chanmanee
(The University of Texas at Arlington Arlington, Texas, United States)
Joseph Fillion
(Jacobs (United States) Dallas, Texas, United States)
Kathryn Ollenburg
(Jacobs (United States) Dallas, Texas, United States)
Shannon McCall
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
February 18, 2024
Publication Date
July 21, 2024
Publication Information
Publisher: International Conference on Environmental Systems
Subject Category
Man/System Technology and Life Support
Report/Patent Number
ICES-2024-168
Meeting Information
Meeting: 53rd International Conference on Environmental Systems (ICES)
Location: Louisville, KY
Country: US
Start Date: July 21, 2024
End Date: July 25, 2024
Sponsors: International Conference on Environmental Systems
Funding Number(s)
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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