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Normal Gravity Testing of a Microchannel Phase Separator for In Situ Resource UtilizationA microchannel separator, with 2.7 millimeters as the smallest dimension, was tested, and a pore throat structure captured and removed liquid from a gas-liquid stream. The microchannel device was tested over a of gas and liquid flow rates ranging from 0.0005 up to 0. 14 volume fraction of liquid. Four liquids were tested with air. The biggest factor affecting the throughput is the capacity of liquid flow through the pore throat, which is dictated by permeability, liquid viscosity, flow area, pore throat thickness, and pressure difference across the pore throat. Typically, complete separation of gas and liquid fractions was lost when the liquid flow rate reached about 40 to 60% of the pore throat capacity. However, this could occur over a range of 10 to 90% utilization of pore throat capacity. Breakthrough occurs in the microchannel phase separator at conditions similar to the annular to plug flow transition of two-phase microgravity pipe flow implying that operating in the proper flow regime is crucial. Analysis indicates that the Bond number did not affect performance, supporting the premise that hydrodynamic, interfacial, and capillary forces are more important than gravity. However, the relative importance of gravity is better discerned through testing under reduced gravity conditions.
Document ID
20010069258
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
TeGrotenhuis, Ward E.
(Battelle Memorial Inst. Richland, WA United States)
Stenkamp, Victoria S.
(Battelle Memorial Inst. Richland, WA United States)
McQuillen, John
Date Acquired
September 7, 2013
Publication Date
June 1, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NAS 1.26:210955
E-12809
NASA/CR-2001-210955
Funding Number(s)
CONTRACT_GRANT: NAS3-00137
CONTRACT_GRANT: RTOP 101-13-0B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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