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Development of a Membrane Based Gas-Liquid Separator for the Space Station Water Processor
Technical Paper
2001-01-2357
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The Water Processor developed for the International Space Station includes a high temperature catalytic reactor that utilizes oxygen gas to oxidize dissolved chemicals. The effluent from the reactor is a mixture of gases (O2, CO2, N2) and hot water. Since the crew has requested that drinking water does not contain any free gas at body temperature (37.8 °C or 100 °F), a phase separator operating at elevated temperatures is required downstream of the catalytic reactor.
For this application, Hamilton Sundstrand Space Systems International (HSSSI) has developed a passive Gas Liquid Separator (GLS) that relies on a positive barrier - a membrane - to extract the free gas from the inlet two-phase mixture. The membrane selected is a hollow fiber hydrophobic asymmetric membrane with pore size in the ultra-filtration range.
This paper outlines the challenges in both design and operation that were overcome during the development of this device.
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Citation
Thibaud-Erkey, C., Lanzarone, A., Lurie, A., Snowdon, D. et al., "Development of a Membrane Based Gas-Liquid Separator for the Space Station Water Processor," SAE Technical Paper 2001-01-2357, 2001, https://doi.org/10.4271/2001-01-2357.Also In
References
- “Polymeric gas separation membranes” 156 Paul, D. R. Yampolski, Y. P. CRC Press 1994