Analysis of Spacecraft Cabin Carbon Dioxide Capture via Deposition

dc.creatorBelancik, Grace
dc.creatorJan, Darrell
dc.creatorHuang, Roger
dc.date.accessioned2018-07-07T22:08:36Z
dc.date.available2018-07-07T22:08:36Z
dc.date.issued2018-07-08
dc.descriptionGrace Belancik, NASA
dc.descriptionDarrell Jan, NASA
dc.descriptionRoger Huang, NASA
dc.descriptionICES302: Physio-chemical Life Support- Air Revitalization Systems -Technology and Process Development
dc.descriptionThe 48th International Conference on Environmental Systems was held in Albuquerque, New Mexico, USA on 08 July 2018 through 12 July 2018.
dc.description.abstractExtended manned missions through deep space present a number of unique challenges yet to be solved before said missions are feasible. One pertinent challenge is the CO2 removal system, as the current state-of-the-art requires repeated, costly maintenance. Multiple alternative CO2 removal systems are currently being evaluated as potential successors, including solid and liquid sorbents. An alternative to sorption techniques entirely is deposition of CO2 from the cabin atmosphere onto a cold surface. Deposition provides numerous benefits, including multiple methods of generating a cold surface. Cryogenic coolers and thermal radiators are two methods that are both highly reliable. Another benefit is the ability to provide humidity and trace contaminant control, as well as CO2 storage and compression, in addition to CO2 capture. Cryogenic coolers, specifically Stirling coolers, are currently being tested for use in Martian atmosphere CO2 capture, but the work described in this paper is one of the first examinations into the application of spacecraft cabin atmosphere. After the Stirling cooler CO2 deposition system was built, a test matrix of varying inlet flow rates, CO2 concentrations, and temperature set points was completed to evaluate the system. In addition, one set of parameters was selected to ensure repeatability and determine a working cycle time. A decaying increase of CO2 removal rate with decreasing temperature was observed at all tested inlet flow rates and concentrations. Also, CO2 removal rate decayed with system run time. The data gleaned from this initial study will be used to inform a more efficient, cycling CO2 deposition system design.en_US
dc.identifier.otherICES_2018_228
dc.identifier.urihttp://hdl.handle.net/2346/74183
dc.language.isoengen_US
dc.publisher48th International Conference on Environmental Systemsen_US
dc.subjectCO2 Removal
dc.subjectCryogenic Cooling
dc.subjectAir Revitalization
dc.subjectLife Support
dc.subjectDeposition
dc.titleAnalysis of Spacecraft Cabin Carbon Dioxide Capture via Depositionen_US
dc.typePresentationen_US

Files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
ICES_2018_228.pdf
Size:
580.87 KB
Format:
Adobe Portable Document Format
Description:

License bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.57 KB
Format:
Item-specific license agreed upon to submission
Description: