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Cryogenic Thermal Emittance Measurements on Small-Diameter Stainless Steel TubingThe Mid Infrared Instrument aboard the James Webb Space Telescoep includes a mechanical cryocooler which cools its detectors to their 6 K operating temperature. The refrigerant flows through several meters of approximately 2 mm diameter 304L stainless steel tubing, with some sections gold plated, and some not, which are exposed to their environment. An issue of water freezing onto the tube surfaces is mitigated by a running a warm gas through the lines to sublimate the water. To model the effect of this process on nearby instruments, an accurate measure of the tube emittance is needed. Previously we reported the abosprtance of the gold plated stainless steel tubing as a function of source temperature (i.e. its environment). In this work the thermal emittance of the uncoated tubing is measured as a function of its temperature between 100 and 300 K. This value leads to an accurate prediction of the minimum length of time required to thermally recycle the system. We report the technique and present the results.
Document ID
20170006544
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Jahromi, A. E.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Tuttle, J. G.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Canavan, E. R.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
July 13, 2017
Publication Date
July 9, 2017
Subject Category
Instrumentation And Photography
Report/Patent Number
GSFC-E-DAA-TN44150
Meeting Information
Meeting: Joint Cryogenic Engineering Conference and International Cryogenic Materials Conference 2017
Location: Madison, WI
Country: United States
Start Date: July 9, 2017
End Date: July 13, 2017
Sponsors: Fermilab Particle Astrophysics Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
cryogenic
stainless steel
thermal emissivity
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