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The Design and Testing of a Fully Redundant Regenerative CO2 Removal System (RCRS) for the Shuttle Orbiter

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2001

Year

Abstract

<div class="htmlview paragraph">Research into increased capacity solid amine sorbents has found a candidate (SA9T) that will provide enough increase in cyclic carbon dioxide removal capacity to produce a fully redundant Regenerative Carbon Dioxide Removal System (RCRS). This system will eliminate the need for large quantities of backup LiOH, thus gaining critical storage space on board the shuttle orbiter. This new sorbent has shown an ability to package two fully redundant (four) sorbent beds together with their respective valves, fans and plumbing to create two operationally independent systems. The increase in CO<sub>2</sub> removal capacity of the new sorbent will allow these two systems to fit within the envelope presently used by the RCRS.</div> <div class="htmlview paragraph">This paper reports on the sub-scale amine testing performed in support of the development effort. In addition, this paper will provide a preliminary design schematic of a fully redundant RCRS.</div>