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Testing of a Miniature Loop Heat Pipe Using a Thermal Electrical Cooler for Temperature ControlThis paper describes the design and testing of a miniature LHP having a 7 mm O.D. evaporator with an integral CC. The vapor line and liquid line are made of 1.6mm stainless steel tubing. The evaporator and the CC are connected on the outer surface by a copper strap and a thermoelectric (TEC) is installed on the strap. The TEC is used to control the CC temperature by applying an electrical current for heating or cooling. Tests performed in ambient included start-up, power cycle, sink temperature cycle, and CC temperature control using TEC. The LHP demonstrated very robust operation in all tests where the heat load varied between 0.5W and 1OOW, and the sink temperature varied between 243K and 293K. The heat leak from the evaporator to the CC was extremely small. The TEC was able to control the CC temperature within +/-0.3K under all test conditions, and the required control heater power was less than 1W.
Document ID
20040074259
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Jeong, Soeng-II
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Butler, Dan
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 34th ICES Conference
Location: Colorado Springs, CO
Country: United States
Start Date: July 19, 2003
End Date: July 22, 2003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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