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Distillation Designs for the Lunar SurfaceGravity-based distillation methods may be applied to the purification of wastewater on the lunar base. These solutions to water processing are robust physical separation techniques, which may be more advantageous than many other techniques for their simplicity in design and operation. The two techniques can be used in conjunction with each other to obtain high purity water. The components and feed compositions for modeling waste water streams are presented in conjunction with the Aspen property system for traditional stage distillation. While the individual components for each of the waste streams will vary naturally within certain bounds, an analog model for waste water processing is suggested based on typical concentration ranges for these components. Target purity levels for recycled water are determined for each individual component based on NASA s required maximum contaminant levels for potable water Optimum parameters such as reflux ratio, feed stage location, and processing rates are determined with respect to the power consumption of the process. Multistage distillation is evaluated for components in wastewater to determine the minimum number of stages necessary for each of 65 components in humidity condensate and urine wastewater mixed streams.
Document ID
20100024236
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Boul, Peter J.
(Engineering Research and Consulting, Inc. Houston, TX, United States)
Lange,Kevin E.
(Jacobs Technologies Engineering Science Contract Group Houston, TX, United States)
Conger, Bruce
(Hamilton Sundstrand Corp. Houston, TX, United States)
Anderson, Molly
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2010
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
JSC-CN-20189
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Barcelona
Country: Spain
Start Date: July 11, 2010
End Date: July 15, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 4300-6/-2/-4
Distribution Limits
Public
Copyright
Public Use Permitted.
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