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The Design and Testing of a Fully Redundant Regenerative CO2 Removal System (RCRS) for the Shuttle Orbiter Hamilton Sundstrand Space Systems International

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Filburn, Tom, author.
Conference Name:
31st International Conference On Environmental Systems (2001-07-09 : Orlando, Florida, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2001
Summary:
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 CO2 removal capacity of the new sorbent will allow these two systems to fit within the envelope presently used by the RCRS.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
Notes:
Vendor supplied data
Publisher Number:
2001-01-2420
Access Restriction:
Restricted for use by site license

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