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Open AccessProceedings Article

Rapid Cycle Amine (RCA 2.0) System Development

TLDR
The Rapid Cycle Amine (RCA) as discussed by the authors is a low-power assembly capable of simultaneously removing carbon dioxide and humidity from an influent air steam and subsequent regeneration when exposed to a vacuum source.
Abstract
The Rapid Cycle Amine (RCA) system is a low-power assembly capable of simultaneously removing carbon dioxide (CO2) and humidity from an influent air steam and subsequent regeneration when exposed to a vacuum source. Two solid amine sorbent beds are alternated between an uptake mode and a regeneration mode. During the uptake mode, the sorbent is exposed to an air steam (ventilation loop) to adsorb CO2 and water (H2O) vapor, whereas during the regeneration mode, the sorbent rejects the adsorbed CO2 and H2O vapor to a vacuum source. The two beds operate such that while one bed is in the uptake mode, the other is in the regeneration mode, thus continuously providing an on-service sorbent bed by which CO2 and humidity may be removed. A novel valve assembly provides a simple means of diverting the process air flow through the uptake bed while simultaneously directing the vacuum source to the regeneration bed. Additionally, the valve assembly is designed to allow for switching between uptake and regeneration modes with only one moving part while minimizing gas volume losses to the vacuum source by means of an internal pressure equalization step during actuation. The process can be controlled by a compact, low-power controller design with several modes of operation available to the user. Together with NASA Johnson Space Center, Hamilton Sundstrand Space Systems International, Inc. has been developing RCA 2.0 based on performance and design feedback on several sorbent bed test articles and valve design concepts. A final design of RCA 2.0 was selected in November 2011 and fabricated and assembled between March and August 2012, with delivery to NASA Johnson Space Center in September 2012. This paper provides an overview of the RCA system design and results of pre-delivery testing.

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Citations
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Continued Development of the Rapid Cycle Amine (RCA) System for Advanced Extravehicular Activity Systems

TL;DR: In this paper, the Rapid Cycle Amine (RCA) Carbon Dioxide (CO2) and Humidity control system has been integrated into an advanced primary life support system (PLSS 2.0) to evaluate the interaction of the RCA among other PLSS components in a ground test environment.

Advanced Supported Liquid Membranes for CO2 Control in Extravehicular Activity Applications

TL;DR: In this article, a supported liquid membrane (SLM) was used to vent CO2 to space for an extravehicular activity (EVA) mission, and the SLM function was demonstrated with representative pressures of CO2, O2, and water (H2O).

Next Generation Life Support Project Status

TL;DR: The Next Generation Life Support (NGLS) project is one of over twenty technology development projects sponsored by NASA's Game Changing Development Program (GCDPP) as mentioned in this paper, with a focus on technologies for future use in spacecraft cabin and space suit applications.

Utilizing a Suited Manikin Test Apparatus and Space Suit Ventilation Loop to Evaluate Carbon Dioxide Washout

TL;DR: A suited manikin test apparatus (SMTA) was developed to augment testing of the portable life support subsystem (PLSS) ventilation loop in order to provide a lower cost and more controlled alternative to human testing.

Continued Advancement of Supported Liquid Membranes for Carbon Dioxide Control in Extravehicular Activity Applications

TL;DR: In this paper, a support liquid membrane (SLM) was used to vent CO2 to space and retain oxygen. But the required performance could be obtained with a supported liquid membrane, which is a microporous material filled with a liquid that selectively reacts with CO2 over O2.
References
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Proceedings ArticleDOI

The Extended Duration Orbiter Regenerable CO Removal System

TL;DR: The regenerative CO2 removal system (RCRS) as mentioned in this paper uses a solid amine material to adsorb carbon dioxide and water vapor and periodically desorb these to space vacuum.
Proceedings ArticleDOI

Development Status of the Carbon Dioxide and Moisture Removal Amine Swing-Bed System (CAMRAS)

TL;DR: In this article, Hamilton Sundstrand has successfully designed, fabricated, tested and delivered three, state-of-the-art, solid amine prototype systems capable of continuous CO2 and humidity removal from a closed, habitable atmosphere.
Book

Advanced Emu Portable Life Support System (Plss) and Shuttle/ISS Emu Schematics: A Comparison

TL;DR: This paper performs a comparison between the Shuttle/ISS EMU PLSS schematic and the Advanced EMUPLSS schematic complete with a discussion for each difference.
Proceedings ArticleDOI

Simulation and Optimization of Vacuum Swing Adsorption Units for Spacesuit Carbon Dioxide and Humidity Control

TL;DR: In this paper, a prototype air revitalization unit employing this technology has been fabricated in both a rectangular and cylindrical geometry and experimental results for these test articles have been collected and are described in detail.
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