Integrated Water Recovery System Test

2003-01-2577

07/07/2003

Event
International Conference On Environmental Systems
Authors Abstract
Content
The work presented in this paper summarizes the performance of subsystems used during an integrated advanced water recovery system test conducted by the Crew and Thermal Systems Division (CTSD) at NASA-Johnson Space Center (JSC). The overall objective of this test was to demonstrate the capability of an integrated advanced water recovery system to produce potable quality water for at least six months. Each subsystem was designed for operation in microgravity. The primary treatment system consisted of a biological system for organic carbon and ammonia removal. Dissolved solids were removed by reverse osmosis and air evaporation systems. Finally, ion exchange technology in combination with photolysis or photocatalysis was used for polishing of the effluent water stream. The wastewater stream consisted of urine and urine flush water, hygiene wastewater and a simulated humidity condensate.
Meta TagsDetails
DOI
https://doi.org/10.4271/2003-01-2577
Pages
16
Citation
Campbell, M., Finger, B., Verostko, C., Wines, K. et al., "Integrated Water Recovery System Test," SAE Technical Paper 2003-01-2577, 2003, https://doi.org/10.4271/2003-01-2577.
Additional Details
Publisher
Published
Jul 7, 2003
Product Code
2003-01-2577
Content Type
Technical Paper
Language
English