Development of Flow Boiling and Condensation Experiment on the International Space Station- Normal and Low Gravity Flow Boiling Experiment Development and Test ResultsFlow boiling and condensation have been identified as two key mechanisms for heat transport that are vital for achieving weight and volume reduction as well as performance enhancement in future space systems. Since inertia driven flows are demanding on power usage, lower flows are desirable. However, in microgravity, lower flows are dominated by forces other than inertia (like the capillary force). It is of paramount interest to investigate limits of low flows beyond which the flow is inertial enough to be gravity independent. One of the objectives of the Flow Boiling and Condensation Flight Experiment sets to investigate these limits for flow boiling and condensation. A two-phase flow loop consisting of a Flow Boiling Module and two Condensation Modules has been developed to experimentally study flow boiling condensation heat transfer in the reduced gravity environment provided by the reduced gravity platform. This effort supports the development of a flow boiling and condensation facility for the International Space Station (ISS). The closed loop test facility is designed to deliver the test fluid, FC-72 to the inlet of any one of the test modules at specified thermodynamic and flow conditions. The zero-g-aircraft tests will provide subcooled and saturated flow boiling critical heat flux and flow condensation heat transfer data over wide range of flow velocities. Additionally, these tests will verify the performance of all gravity sensitive components, such as evaporator, condenser and accumulator associated with the two-phase flow loop. We will present in this paper the breadboard development and testing results which consist of detailed performance evaluation of the heater and condenser combination in reduced and normal gravity. We will also present the design of the reduced gravity aircraft rack and the results of the ground flow boiling heat transfer testing performed with the Flow Boiling Module that is designed to investigate flow boiling heat transfer and Critical Heat Flux (CHF) phenomena.
Document ID
20150002329
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Nahra, Henry K. (NASA Glenn Research Center Cleveland, OH United States)
Hall, Nancy R. (NASA Glenn Research Center Cleveland, OH United States)
Hasan, Mohammad M. (NASA Glenn Research Center Cleveland, OH United States)
Wagner, James D. (NASA Glenn Research Center Cleveland, OH United States)
May, Rochelle L. (NASA Glenn Research Center Cleveland, OH United States)
Mackey, Jeffrey R. (Vantage Partners, LLC Brook Park, OH, United States)
Kolacz, John S. (NASA Glenn Research Center Cleveland, OH United States)
Butcher, Robert L. (NASA Glenn Research Center Cleveland, OH United States)
Frankenfield, Bruce J. (NASA Glenn Research Center Cleveland, OH United States)
Mudawar, Issam (Purdue Univ. South Bend, IN, United States)
Konichi, Chris (Purdue Univ. South Bend, IN, United States)
Hyounsoon, Lee (Purdue Univ. South Bend, IN, United States)
Date Acquired
March 3, 2015
Publication Date
November 3, 2013
Subject Category
Spacecraft Design, Testing And PerformanceFluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN11720Report Number: GRC-E-DAA-TN11720
Meeting Information
Meeting: International Symposium for Physical Sciences in Space
Location: Orlando, FL
Country: United States
Start Date: November 3, 2013
End Date: November 8, 2013
Sponsors: American Society for Gravitational and Space Research