Design and Modeling of a Radiator with Digital Turn-Down Capability under Variable Heat Rejection Requirements

Author:

Miller Jennifer1,Birur Gajanana1,Ganapathi Gani1,Sunada Eric1,Berisford Daniel1,Stephan Ryan2

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology

2. NASA Johnson Space Center

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. 4Bannon,E.T.,Bower,B.E.,Sheth,R.,Stephan,R.,Chandrasekhar,P.andZay,B. "ElectrochromicRadiator Coupon Level Testingand FullScale ThermalMathModeling for use on Altair Lunar Lander." AIAA International Conference onEnvironmental Systems, AIAA-2010-6110.July2010.

2. 5Lillibridge,S.T."FreezableRadiatorTestReport,"CTSD-ADV-743,CTSD,January27,2011.

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1. Effect of Gravity on Ice-Layer Growth in a Freezable Heat Exchanger;Journal of Thermophysics and Heat Transfer;2016-07

2. Compact Heat Rejection System Utilizing Integral Variable Conductance Planar Heat Pipe Radiator for Space Application;Gravitational and Space Research;2015-12-01

3. Overview of NASA's Thermal Control Technology Development for Exploraton Project;41st International Conference on Environmental Systems;2011-07-17

4. Fluid Line Evacuation and Freezing Experiments for Digital Radiator Concept;41st International Conference on Environmental Systems;2011-07-17

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