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Testing of a Neon Loop Heat Pipe for Large Area CryocoolingCryocooling of large areas such as optics, detector arrays, and cryogenic propellant tanks is required for future NASA missions. A cryogenic loop heat pipe (CLHP) can provide a closed-loop cooling system for this purpose and has many advantages over other devices in terms of reduced mass, reduced vibration, high reliability, and long life. A neon CLHP was tested extensively in a thermal vacuum chamber using a cryopump as the heat sink to characterize its transient and steady performance and verify its ability to cool large areas or components. Tests conducted included loop cool-down from the ambient temperature, startup, power cycle, heat removal capability, loop capillary limit and recovery from a dry-out, low power operation, and long duration steady state operation. The neon CLHP demonstrated robust operation. The loop could be cooled from the ambient temperature to subcritical temperatures very effectively, and could start successfully by applying power to both the pump and evaporator without any pre-conditioning. It could adapt to changes in the pump power andor evaporator power, and reach a new steady state very quickly. The evaporator could remove heat loads between 0.25W and 4W. When the pump capillary limit was exceeded, the loop could resume its normal function by reducing the pump power. Steady state operations were demonstrated for up to 6 hours. The ability of the neon loop to cool large areas was therefore successfully verified.
Document ID
20140005419
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Robinson, Franklin Lee
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
May 9, 2014
Publication Date
March 25, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
GSFC-E-DAA-TN13549
Report Number: GSFC-E-DAA-TN13549
Meeting Information
Meeting: 2014 Spacecraft Thermal Control Workshop
Location: El Segundo, CA
Country: United States
Start Date: March 25, 2014
End Date: March 27, 2014
Sponsors: The Aerospace Corporation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Cryogenics
Loop Heat Pipes
Cryocooling
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