Compact and lightweight sabatier reactor for carbon dioxide reduction
Open accessAbstract
The utilization of CO2 to produce life support consumables, such as O2 and H2O, via the Sabatier reaction is an important aspect of NASA s cabin Atmosphere Revitalization System and In-Situ Resource Utilization architectures for both low-earth orbit and long-term manned space missions. In the current International Space Station (ISS) and other low orbit missions, metabolically-generated CO2 is removed from the cabin air and vented into space, resulting in a net loss of O2. This requires a continuous resupply of O2 via water electrolysis, and thus highlights the need for large water storage capacity. For long-duration space missions, the amount of life support consumables is limited and resupply options are practically nonexistent, thus atmosphere resource management and recycle becomes crucial to significantly reduce necessary O2 and H2O storage. Additionally, the potential use of the Martian CO2-rich atmosphere and Lunar regolith to generate life support consumables and propellant fuels is of interest to NASA. Precision Combustion, Inc. (PCI) has developed a compact, lightweight Microlith(Registered TradeMark)-based Sabatier (CO2 methanation) reactor which demonstrates the capability of achieving high CO2 conversion and near 100% CH4 selectivity at space velocities of 30,000-60,000 hr-1. The combination of the Microlith(Registered TradeMark) substrates and durable, novel catalyst coating permitted efficient Sabatier reactor operation that favors high reactant conversion, high selectivity, and long-term durability. This paper presents the reactor development and performance results at various operating conditions. Additionally, results from 100-hr durability tests and mechanical vibration tests are discussed.
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Even nowadays, all methods used for air revitalization are physicochemical and not regenerative.
“So even nowadays, all of the methods used for air revitalization are physicochemical and not regenerative (Junaedi et al., 2011; Tobias et al., 2011).”
From Use of Photobioreactors in Regenerative Life Support Systems for Human Space Exploration (2021) · cites this paper as Junaedi et al., 2011
The Introduction (indexed as section C; page not supplied) says that the ISS and other low-orbit missions vent removed CO₂, causing a net loss of oxygen. That supports a limited claim about those missions, not the assertion that all air-revitalization methods are nonregenerative: the same section describes a closed-loop system that recycles CO₂ into water and can substantially close the oxygen loop. (LLM, conf=0.86)
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- Authors
- Junaedi, C., Hawley, K., Walsh, D., Roychoudhury, S., Abney, M., & Perry, J.
- Affiliations
- Precision Combustion (United States) (US)
- Marshall Space Flight Center (US)
- Venue
- 41st International Conference on Environmental Systems
- Published
- 2011-07-17
- OpenAlex
- W2068759931
- Cited by
- 49
- References
- 25
- Citations by year
- 2025: 3 · 2024: 7 · 2023: 4 · 2022: 4 · 2021: 9 · 2020: 4 · 2018: 8 · 2017: 1 · 2016: 1 · 2015: 1 · 2014: 2 · 2013: 2 · 2012: 2
- FWCI
- 10.36
- Type
- conference paper
- Language
- en
- Open access
- green
- hdl.handle.net
- Locations
- International Conference on Environmental Systems (ICES) (publishedVersion)
- NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
- Funders
- National Aeronautics and Space Administration
- Marshall Space Flight Center
- Topics
- Physical Sciences › Chemical Engineering › Catalysis › Catalysts for Methane Reforming
- Physical Sciences › Materials Science › Materials Chemistry › Catalytic Processes in Materials Science
- Physical Sciences › Energy › Renewable Energy, Sustainability and the Environment › CO2 Reduction Techniques and Catalysts
- Keywords
- CO2 methanation, in-situ resource utilization, oxygen production, water production, methane selectivity, catalyst stability, catalyst coating, vibration testing, Mars atmosphere, lunar regolith, long-duration spaceflight
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