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Extended duration orbiter study: CO2 removal and water recoveryTwo electrochemical depolarized carbon dioxide concentrator subsystems were evaluated against baseline lithium hydroxide for (1) the baseline orbiter when expanded to accommodate a crew of seven (mission option one), (2) an extended duration orbiter with a power extension package to reduce fuel cell expendables (mission option two), and (3) an extended duration orbiter with a full capability power module to eliminate fuel cell expendables (mission option three). The electrochemical depolarized carbon dioxide concentrator was also compared to the solid amine regenerable carbon dioxide removal concept. Water recovery is not required for Mission Option One since sufficient water is generated by the fuel cells. The vapor compression distillation subsystem was evaluated for mission option two and three only. Weight savings attainable using the vapor compression distillation subsystem for water recovery versus on-board water storage were determined. Combined carbon dioxide removal and water recovery was evaluated to determine the effect on regenerable carbon dioxide removal subsystem selection.
Document ID
19800002555
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Marshall, R. D.
(Life Systems, Inc. Cleveland, OH, United States)
Ellis, G. S.
(Life Systems, Inc. Cleveland, OH, United States)
Schubert, F. H.
(Life Systems, Inc. Cleveland, OH, United States)
Wynveen, R. A.
(Life Systems, Inc. Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1979
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LSI-ER-319-24
NASA-CR-160317
Report Number: LSI-ER-319-24
Report Number: NASA-CR-160317
Accession Number
80N10800
Funding Number(s)
CONTRACT_GRANT: NAS9-15218
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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