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Thermal Vacuum Test of Ice as a Phase Change Material Integrated with a RadiatorWater may be used as radiation shielding for Solar Particle Events (SPE) to protect crewmembers in the Lunar Electric Rover (LER). Because the water is already present for radiation protection, it could also provide a mass efficient solution to the vehicle's thermal control system. This water can be frozen by heat rejection from a radiator and used as a Phase Change Material (PC1V1) for thermal storage. Use of this water as a PCM can eliminate the need for a pumped fluid loop thermal control system as well as reduce the required size of the radiator. This paper describes the testing and analysis performed for the Rover Engineering Development Unit (REDU), a scaled-down version of a water PCM heat sink for the LER. The REDU was tested in a thermal-vacuum chamber at environmental temperatures similar to those of a horizontal radiator panel on the lunar surface. Testing included complete freeze and melt cycles along with scaled transient heat load profiles simulating a 24-hour day for the rover.
Document ID
20100016331
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Lee, Steve A.
(MEI Technologies, Inc. Houston, TX, United States)
Leimkuehler, Thomas O.
(Paragon Space Corp. Houston, TX, United States)
Stephan, Ryan
(NASA Johnson Space Center Houston, TX, United States)
Le, Hung V.
(Geo Controls Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
JSC-CN-20213
Report Number: JSC-CN-20213
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Barcelona
Country: Spain
Start Date: July 11, 2010
End Date: July 15, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 119103
Distribution Limits
Public
Copyright
Public Use Permitted.
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