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Characterization of an Improved Solid Amine for a Regenerative CO2 Removal System NASA Johnson Space Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Graf, J. C., author.
Conference Name:
International Conference On Environmental Systems (1993-07-12 : Colorado Springs, Colorado, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1993
Summary:
The Shuttle Orbiter humidity control and carbon dioxide removal system for extended duration missions presently uses a solid amine called HS-C. This August, on board STS-62, a new solid amine called HS-C+ will be used. HS-C+ uses the same amine and the substrate material, but a different preparation process. Forty-seven breakthrough tests have been conducted to characterize the performance of HS-C+. CO2 partial pressure, bed temperature, and H2O partial pressure were varied. Eleven HS-C breakthrough tests were also run to provide a direct comparison. Under all conditions tested, HS-C+ outperformed HS-C. Both materials adsorb all CO2 and H2O available at the start of a test when the beds are fully desorbed. As the bed becomes partially loaded, the CO2 and H2O adsorption rates decrease rapidly. HS-C+ continues adsorbing all CO2 and H2O available for a longer time. Greater surface area on HS-C+ may cause the improved performance
Notes:
Vendor supplied data
Publisher Number:
932292
Access Restriction:
Restricted for use by site license

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