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Development of the Two Phase Flow Separator Experiment for a Reduced Gravity Aircraft FlightThe recent hardware development and testing of a reduced gravity aircraft flight experiment has provided valuable insights for the future design of the Two Phase Flow Separator Experiment (TPFSE). The TPFSE is scheduled to fly within the Fluids Integration Rack (FIR) aboard the International Space Station (ISS) in 2020. The TPFSE studies the operational limits of gas and liquid separation of passive cyclonic separators. A passive cyclonic separator utilizes only the inertia of the incoming flow to accomplish the liquid-gas separation. Efficient phase separation is critical for environmental control and life support systems, such as recovery of clean water from bioreactors, for long duration human spaceflight missions. The final low gravity aircraft flight took place in December 2015 aboard NASA's C9 airplane.
Document ID
20170001403
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Golliher, Eric
(NASA Glenn Research Center Cleveland, OH United States)
Gotti, Daniel
(Universities Space Research Association Cleveland, OH, United States)
Owens, Jay
(Universities Space Research Association Cleveland, OH, United States)
Gilkey, Kelly
(NASA Glenn Research Center Cleveland, OH United States)
Pham, Nang
(NASA Glenn Research Center Cleveland, OH United States)
Stehno, Philip
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 8, 2017
Publication Date
June 13, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN32232
Report Number: GRC-E-DAA-TN32232
Meeting Information
Meeting: AIAA Thermophysics Conference 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC13BA10B
WBS: WBS 904211.04.20.14
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
fluid mechanics
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