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William Papale

Researcher at UTC Aerospace Systems

Publications -  3
Citations -  17

William Papale is an academic researcher from UTC Aerospace Systems. The author has contributed to research in topics: Sorbent & Control theory. The author has an hindex of 2, co-authored 3 publications receiving 17 citations.

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Proceedings Article

Rapid Cycle Amine (RCA 2.0) System Development

TL;DR: 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.

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.

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

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 was delivered to NASA in 2006 and was notated as RCA 10 and sized for the extravehicular activity (EVA) The new 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 operation of the RCA so that while one bed is in adsorb (uptake) mode, the other is in the desorb (regeneration) mode The RCA has now 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 10, RCA 20, and RCA 30 The RCA 30 was the most recent RCA fabrication and was delivered to NASA-JSC in June 2015 The RCA 10 test article was designed with a pneumatically actuated linear motion spool valve The RCA 20 and 30 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 20 and 30 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 overreview of the design and development of RCA 10, 20 and 30 including detail differences between the design specifications of each