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Testing of a Miniature Loop Heat Pipe with Multiple Evaporators and Multiple Condensers for Space ApplicationsThermal performance of a miniature loop heat pipe (MLHP) with two evaporators and two condensers is described. A comprehensive test program, including start-up, high power, low power, power cycle, and sink temperature cycle tests, has been executed at NASA Goddard Space Flight Center for potential space applications. Experimental data showed that the loop could start with heat loads as low as 2W. The loop operated stably with even and uneven evaporator heat loads, and even and uneven condenser sink temperatures. Heat load sharing between the two evaporators was also successfully demonstrated. The loop had a heat transport capability of l00W to 120W, and could recover from a dry-out by reducing the heat load to evaporators. Low power test results showed the loop could work stably for heat loads as low as 1 W to each evaporator. Excellent adaptability of the MLHP to rapid changes of evaporator power and sink temperature were also demonstrated.
Document ID
20070032906
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Nagano, Hosei
(Japan Aerospace Exploration Agency Japan)
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 23, 2013
Publication Date
September 24, 2006
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 8th International Heat Pipe Symposium
Location: Kumamoto
Country: Japan
Start Date: September 24, 2006
End Date: September 27, 2006
Distribution Limits
Public
Copyright
Public Use Permitted.
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