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Thermal Vacuum Test Performance of the Hubble Space Telescope (HST) Wide Field Camera 3 (WFC3) Variable Conductance Heat Pipe AssemblyThe Variable Conductance Heat Pipe (VCHP) Assembly of the HST Wide Field Camera 3 was subjected to thermal vacuum (TN) environmental testing. The test program included both maximum and minimum environments as well as simulated on-orbit cycling. Elements of the VCHP assembly included a VCHP, an optical bench cold plate with an imbedded constant conductance heat pipe, and a VCHP reservoir radiator with a proportionally controlled heater. The purpose of the test was to characterize and demonstrate the assembly s ability to control the temperature of the cold plate, which provides a stable thermal environment for the instrument s optical bench. This paper discusses the VCHP Assembly control performance and control authority during the dynamic hot and cold 90-minute orbit cycling test phases.
Document ID
20030053443
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cleveland, Paul E.
(Energy Solutions International, LLC United States)
Buchko, Matthew T.
(Swales Aerospace United States)
Stavely, Richard A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Quality Assurance And Reliability
Report/Patent Number
SAE-2003-01-2459
Report Number: SAE-2003-01-2459
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Vancouver, British Columbia
Country: Canada
Start Date: July 7, 2003
End Date: July 10, 2003
Sponsors: Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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