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Bosch CO2 Reduction System DevelopmentRefinements in the design of a Bosch CO2 reduction unit for spacecraft O2 production are described. Sealing of the vacuum insulation jacket was simplified so that high vacuum and high insulation performance are easily maintained. The device includes a relatively simple concentric shell recuperative heat exchanger which operates at approximately 95% temperature effectiveness and helps lower power consumption. The influence of reactor temperature, pressure, and recycle gas composition on power consumption was investigated. In general, precise control is not required since power consumption is not very sensitive to moderate variations of these parameters near their optimum values. There are two process rate control modes which match flow rate to process demand. Catalyst conditioning, support, and packing pattern developments assure consistent starts, reduced energy consumption, and extended cartridge life. Operation levels for four or five men were maintained with overall power input values of 50 to 60 watts per man.
Document ID
19750025653
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holmes, R. F.
(General Dynamics/Convair San Diego, CA, United States)
King, C. D.
(General Dynamics/Convair San Diego, CA, United States)
Keller, E. E.
(General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-143959
CASD-NAS-75-030
IR-3
Report Number: NASA-CR-143959
Report Number: CASD-NAS-75-030
Report Number: IR-3
Accession Number
75N33726
Funding Number(s)
CONTRACT_GRANT: NAS8-27276
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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