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Definition of two-phase flow behaviors for spacecraft designData for complete models of two-phase flow in microgravity are taken from in-flight experiments and applied to an adiabatic flow-regime analysis to study the feasibility of two-phase systems for spacecraft. The data are taken from five in-flight experiments by Hill et al. (1990) in which a two-phase pump circulates a freon mixture and vapor and liquid flow streams are measured. Adiabatic flow regimes are analyzed based on the experimental superficial velocities of liquid and vapor, and comparisons are made with the results of two-phase flow regimes at 1 g. A motion analyzer records the flow characteristics at a rate of 1000 frames/sec, and stratified flow regimes are reported at 1 g. The flow regimes observed under microgravitational conditions are primarily annular and include slug and bubbly-slug regimes. The present data are of interest to the design and analysis of two-phase thermal-management systems for use in space missions.
Document ID
19920071659
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reinarts, Thomas R.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Best, Frederick R.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Miller, Katherine M.
(Texas A & M University College Station, United States)
Hill, Wayne S.
(Foster-Miller, Inc. Waltham, MA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Space Nuclear Power Systems Symposium
Location: Albuquerque, NM
Country: United States
Start Date: January 6, 1991
End Date: January 10, 1991
Accession Number
92A54283
Distribution Limits
Public
Copyright
Other

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