Paul B. Reid,1 Vladimir Kradinov,1 Mark D. Freeman,1 Nathan L. Bishop,2 Casey DeRoohttps://orcid.org/0000-0002-9184-4561,3 Thomas N. Jackson,2 Vanessa Marquez,1 Mohit M. Tendulkar,2 Quyen Tran,2 Susan Trolier-McKinstry2
1Harvard-Smithsonian Ctr. for Astrophysics (United States) 2Materials Research Institute, The Pennsylvania State Univ. (United States) 3The Univ. of Iowa (United States)
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Adjustable X-ray optics represent a potential mirror technology for the NASA Lynx X-ray observatory mission concept. Adjustable optics employ an integrated micron-thick piezoelectric film deposited on the convex side of silicon Wolter-type mirror segments. Discrete, independently addressable electrodes on the convex surface form individual actuators; the applied voltages are used to correct the shape of the mirror segments for figure errors resulting from a change in thermal environment, epoxy creep, or failure of an epoxy bond.
On-orbit correction requires a metrology system to provide real-time feedback of mirror figure. We are examining the use of deposited semiconductor strain gauges to monitor mirror mechanical strains and surface temperatures. To establish requirements for monitoring we modeled a variety of thermal and mechanical disturbances to a mirror segment such as might occur on-orbit or from launch. Models are described and resulting requirements and performance discussed.
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Paul B. Reid, Vladimir Kradinov, Mark D. Freeman, Nathan L. Bishop, Casey DeRoo, Thomas N. Jackson, Vanessa Marquez, Mohit M. Tendulkar, Quyen Tran, Susan Trolier-McKinstry, "Strain gauging for on-orbit figure monitoring of adjustable X-ray optics: systems analyses," Proc. SPIE 11822, Optics for EUV, X-Ray, and Gamma-Ray Astronomy X, 1182214 (1 August 2021); https://doi.org/10.1117/12.2595160