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Temperature Oscillations in Loop Heat Pipes - A RevisitThree types of temperature oscillation have been observed in the loop heat pipes. The first type is an ultra-high frequency temperature oscillation with a period on the order of seconds or less. This type of temperature oscillation is of little significance in spacecraft thermal control because the amplitude is in the noise level. The second type is a high frequency, low amplitude temperature oscillation with a period on the order of seconds to minutes and an amplitude on the order of one Kelvin. It is caused by the back-and-forth movement of the vapor front near the inlet or outlet of the condenser. The third type is a low frequency, high amplitude oscillation with a period on the order of hours and an amplitude on the order of tens of Kelvin. It is caused by the modulation of the net heat load into the evaporator by the attached large thermal mass which absorbs and releases energy alternately. Several papers on LHP temperature oscillation have been published. This paper presents a further study on the underlying physical processes during the LHP temperature oscillation, with an emphasis on the third type of temperature oscillation. Specifically, equations governing the thermal and hydraulic behaviors of LHP operation will be used to describe interactions among LHP components, heat source, and heat sink. The following sequence of events and their interrelationship will also be explored: 1) maxima and minima of reservoir and thermal mass temperatures; 2) the range of the vapor front movement inside the condenser; 3) rates of change of the reservoir and thermal mass temperatures; 4) the rate of heat absorption and heat release by the thermal mass and the rate of vapor front movement; and 5) inflection points of the reservoir and thermal mass temperatures.
Document ID
20180002076
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
March 23, 2018
Publication Date
March 20, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Engineering (General)
Report/Patent Number
GSFC-E-DAA-TN52767
Meeting Information
Meeting: Spacecraft Thermal Control Workshop
Location: El Segundo, CA
Country: United States
Start Date: March 20, 2018
End Date: March 22, 2018
Sponsors: Aerospace Corp.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Fluid Mechanics and Thermodynamics
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