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Loop Heat Pipe Operation Using Heat Source Temperature for Set Point ControlLoop heat pipes (LHPs) have been used for thermal control of several NASA and commercial orbiting spacecraft. The LHP operating temperature is governed by the saturation temperature of its compensation chamber (CC). Most LHPs use the CC temperature for feedback control of its operating temperature. There exists a thermal resistance between the heat source to be cooled by the LHP and the LHP's CC. Even if the CC set point temperature is controlled precisely, the heat source temperature will still vary with its heat output. For most applications, controlling the heat source temperature is of most interest. A logical question to ask is: "Can the heat source temperature be used for feedback control of the LHP operation?" A test program has been implemented to answer the above question. Objective is to investigate the LHP performance using the CC temperature and the heat source temperature for feedback control
Document ID
20110013401
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Paiva, Kleber
(Federal Univ. Florianopolis, Santa Catarina, Brazil)
Mantelli, Marcia
(Federal Univ. Florianopolis, Santa Catarina, Brazil)
Date Acquired
August 25, 2013
Publication Date
March 8, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC.CPR.4607.2011
Report Number: GSFC.CPR.4607.2011
Meeting Information
Meeting: 2011 Spacecraft Thermal Control Workshop
Location: ElSegundo, CA
Country: United States
Start Date: March 7, 2011
End Date: March 10, 2011
Distribution Limits
Public
Copyright
Public Use Permitted.
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