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Phase Change Material for Temperature Control of Loop Heat Pipe Compensation ChamberThe compensation chamber (CC) of a loop heat pipe (LHP) requires a stable temperature. In the current technology, the CC is commonly cold biased by exposing it to deep space, and active heater control is used to maintain its temperature stable. Heater power required for a typical LHP with a 300 W heat transport capacity is as much as 25 W. If multiple LHPs are used, heater power requirement could be a bigger issue. Also heater controller or temperature sensor failure could lead to a LHP or mission failure. This paper presents an innovative concept of using phase change material (PCM) for temperature control of LHP CC. Some of the electronics and/or detector assembly waste heat is stored in the PCM and transferred to the LHP CC by constant conductance heat pipes (CCHPs). Phase change of the PCM occurs at a constant temperature and maintains the LHP CC temperature stable. It eliminates heater power and active heater control for the CC. It also increases the reliability of LHP.
Document ID
20120015405
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Choi, Michael K.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 26, 2013
Publication Date
July 29, 2012
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC.CP.7026-2012
Report Number: GSFC.CP.7026-2012
Meeting Information
Meeting: 10th International Energy Conversion Engineering Conference (IECEC)
Location: Atlanta, GA
Country: United States
Start Date: July 29, 2012
End Date: August 1, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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