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Desiccant humidity control system. [for space shuttle cabins
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kester, F. L. Lunde, P. J. |
| Copyright Year | 1975 |
| Description | A 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. |
| File Size | 66632692 |
| Page Count | 345 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750009025 |
| Archival Resource Key | ark:/13960/t25b4w882 |
| Language | English |
| Publisher Date | 1975-06-01 |
| Access Restriction | Open |
| Subject Keyword | Man/system Technology And Life Support Life Support Systems Performance Tests Metabolic Wastes Desiccants Dehumidification Space Shuttles Spacecraft Cabin Atmospheres Carbon Dioxide Human Factors Engineering Water Vapor Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |