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Membrane Separation of Gases from the Martian AtmosphereA test bed has been constructed to test membrane modules for separation of gases under temperature and pressure conditions normally encountered on the surface of Mars. The test bed allows independent control of: (1) feed flow rates, (2) feed composition, (3) feed pressure, (4) permeate pressure, and (5) operating temperature. Preliminary data obtained at a nominal feed pressure of 760 torr and permeate pressure of 10 torr has demonstrated the ability of one membrane module to operate at temperatures as low as -70 C. At temperatures below -40 C, however, significant loss of carbon dioxide and argon was observed, probably indicating condensation at the relatively high pressure used. As expected, permeation flow rates decreased with decreasing temperature, the flow at -30 C approximately 37% of the value at +23 C. Values of permeability for individual gas components showed similar decreases with decreasing temperature, but permeability ratios changed significantly. For example, the ratio of the permeabilities of carbon dioxide and nitrogen increased from 2.6 at 23 C to 5.6 at -30 C. Additional data at lower operating pressures and temperatures must be obtained in order to optimize design of a usable separation system.
Document ID
20030002458
Acquisition Source
Kennedy Space Center
Document Type
Other
Authors
Jennings, Paul A.
(Florida Inst. of Tech. FL United States)
Date Acquired
August 21, 2013
Publication Date
June 1, 2002
Publication Information
Publication: 2000 Final Administrative Report NASA/ASEE Summer Faculty Fellowship Program
Subject Category
Inorganic, Organic And Physical Chemistry
Funding Number(s)
CONTRACT_GRANT: NAG10-280
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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