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A Solid-State Compressor for Integration of CO2 Removal and Reduction AssembliesIntegration of CO2 removal and reduction assemblies in a spacecraft air revitalization system requires an interface with the functionality of a vacuum pump/compressor and a buffer tank. The compressor must meet the vacuum needs of the CO2 removal unit and the pressure needs of the CO2 reduction device, and must also store sufficient CO2 to accommodate the differences in cycle times of the two processes. In this presentation, we describe the design and operation of an adsorption-based device sized for use on the International Space Station. The adsorption compressor functions at a power level approximately ten times lower than a comparable mechanical compression/buffer tank system. The unit is also smaller, lighter, and quieter than its mechanical counterpart.
Document ID
20000121128
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Mulloth, Lila M.
(Lockheed Martin Engineering and Science Services Moffett Field, CA United States)
Finn, John E.
(NASA Ames Research Center Moffett Field, CA United States)
Lung, Bernadette
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Subject Category
Man/System Technology And Life Support
Meeting Information
Meeting: Environmental Systems
Location: Toulouse
Country: France
Start Date: July 10, 2000
End Date: July 13, 2000
Funding Number(s)
PROJECT: RTOP 131-20-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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