Design and Development Comparison of Rapid Cycle Amine 1.0, 2.0, and 3.0

Date

2016-07-10

Journal Title

Journal ISSN

Volume Title

Publisher

46th International Conference on Environmental Systems

Abstract

The development of the Rapid Cycle Amine (RCA) swing-bed technology for carbon dioxide (CO2) removal has been in progress since favorable results were published in 1996. Shortly thereafter, a prototype was designed, developed, and tested successfully and delivered to Johnson Space Center in 1999. An improved prototype (RCA 1.0) was delivered to NASA in 2006 and sized for the extravehicular activity (EVA). The RCA swing-bed technology is a regenerative system which employs two alternating solid-amine sorbent beds to remove CO2 and water. The two-bed design employs a chemisorption process whereby the beds alternate between adsorbtion and desorbsion. This process provides for an efficient RCA operation so that while one bed is in adsorb (uptake) mode, the other is in the desorb (regeneration) mode. The RCA has progressed through several iterations of technology readiness levels. Test articles have now been designed, developed, and tested for the advanced space suit portable life support system (PLSS) including RCA 1.0, RCA 2.0, and RCA 3.0. The RCA 3.0 was the most recent RCA fabrication and was delivered to NASA-JSC in June 2015. The RCA 1.0 test article was designed with a pneumatically actuated linear motion spool valve. The RCA 2.0 and 3.0 test articles were designed with a valve assembly which allows for switching between uptake and regeneration modes while minimizing gas volume losses to the vacuum source. RCA 2.0 and 3.0 also include an embedded controller design to control RCA operation and provide the capability of interfacing with various sensors and other ventilation loop components. The RCA technology is low power, small, and has fulfilled all test requirements levied upon the technology during development testing thus far. This paper will provide an overview of the design and development of RCA 1.0, 2.0 and 3.0 including detail differences between the design specifications of each.

Description

United States
NASA JSC
NASA
UTC Aerospace Systems
ATK/JSC Engineering, Technology, and Science Contract
Jacobs Technology
402
ICES402: Extravehicular Activity: PLSS Systems
Vienna, Austria
Cinda Chullen, NASA Johnson Space Center, USA
Colin Campbell, NASA Johnson Space Center, USA
William Papale, UTC Aerospace Systems, USA
Sean Murray, UTC Aerospace Systems, USA
Robert Wichowski, UTC Aerospace Systems, USA
Bruce Conger, Jacobs, USA
Summer McMillin, Jacobs, USA

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Keywords

Rapid Cycle Amine (RCA), swing-bed technology, carbon dioxide (CO2)removal, regenerative system, solid-amine, sorbent beds, adsorb, desorb, uptake mode, regeneration mode, embedded controller, spool valve

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