Testing of an Amine-Based Pressure-Swing System for Carbon Dioxide and Humidity Control

Abstract

In a crewed spacecraft environment, atmospheric carbon dioxide (CO 2 ) and moisture control is crucial. Hamilton Sundstrand has developed a stable and efficient aminebased CO 2 and water vapor sorbent, SA9T, that is wellsuited for use in a spacecraft environment. The sorbent is efficiently packaged in pressure-swing regenerable beds that are thermally linked to improve removal efficiency and minimize vehicle thermal loads. Flows are all controlled with a single spool valve. This technology has been baselined for the new Orion spacecraft. However, more data was needed on the operational characteristics of the package in a simulated spacecraft environment. A unit was therefore tested with simulated metabolic loads in a closed chamber at Johnson Space Center during the last third of 2006. Tests were run at a variety of cabin temperatures and with a range of operating conditions varying cycle time, vacuum pressure, air flow rate, and crew activity levels. Results of this testing are presented and potential flight operational strategies discussed.