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Effects of Forged Stock and Pure Aluminum Coating on Cryogenic Performance of Heat Treated Aluminum MirrorsIn spite of its baseline mechanical stress relief, aluminum 6061-T651 harbors some residual stress that may relieve and distort mirror figure to unacceptable levels at cryogenic operating temperatures unless relieved during fabrication. Cryogenic instruments using aluminum mirrors for both ground-based and space IR astronomy have employed a variety of heat treatment formulae, with mixed results. We present the results of an on-going test program designed to empirically determine the effects of different stress relief procedures for aluminum mirrors. Earlier test results identified a preferred heat treatment for flat and spherical mirrors diamond turned from blanks cut out of Al6061-T651 plate stock. Further tests have been performed on mirrors from forged stock and one set from plate stock coated with Alumiplate(TM) aluminum coating to measure the effect of these variables on cryogenic performance. The mirrors are tested for figure error and radius of curvature at room temperature and at 80 K for three thermal cycles. We correlate the results of our optical testing with heat treatment and metallographic data.
Document ID
20040033369
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Toland, Ronald
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Ohl, Raymond G.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Barthelmy, Michael P.
(Swales Aerospace Beltsville, MD, United States)
Zewari, S. Wahid
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Greenhouse, Matthew A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
MacKenty, John W.
(Space Telescope Science Inst. Baltimore, MD, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Mechanical Engineering
Meeting Information
Meeting: SPIE-Optical Science and Technology Annual Meeting
Location: San Diego, CA
Country: United States
Start Date: August 3, 2003
End Date: August 8, 2003
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Other

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