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Desiccant humidity control systemA water vapor and carbon dioxide sorbent material (designated HS-C) was developed for potential application to the space shuttle and tested at full scale. Capacities of two percent for carbon dioxide and four percent for water vapor were achieved using space shuttle cabin adsorption conditions and a space vacuum for desorption. Performance testing shows that water vapor can be controlled by varying the air process flow, while maintaining the ability to remove carbon dioxide. A 2000 hour life test was successfully completed, as were tests for sensitivity to cleaning solvent vapors, vibration resistance, and flammability. A system design for the space shuttle shows a 200 pound weight advantage over competitive systems and an even larger advantage for longer missions.
Document ID
19750009025
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lunde, P. J.
(Hamilton Standard Div., United Aircraft Corp. Windsor Locks, CT, United States)
Kester, F. L.
(Hamilton Standard Div., United Aircraft Corp. Windsor Locks, CT, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-115568
SVHSER-6040
Report Number: NASA-CR-115568
Report Number: SVHSER-6040
Accession Number
75N17097
Funding Number(s)
CONTRACT_GRANT: NAS9-11971
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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