Space Telescopes and Instrumentation I: Optical, Infrared, and Millimeter 2006
DOI: 10.1117/12.672926
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An overview of optical fabrication of the JWST mirror segments at Tinsley

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Cited by 13 publications
(13 citation statements)
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“…[ 133,134 ] The infrared scanning Shack–Hartmann test was employed for surface metrology during optical fabrication of James Webb Space Telescope (JWST) segment mirrors before transition to visible interferometry with CGH nulls. [ 135 ]…”
Section: Non‐interferometric Areal Measurementmentioning
confidence: 99%
“…[ 133,134 ] The infrared scanning Shack–Hartmann test was employed for surface metrology during optical fabrication of James Webb Space Telescope (JWST) segment mirrors before transition to visible interferometry with CGH nulls. [ 135 ]…”
Section: Non‐interferometric Areal Measurementmentioning
confidence: 99%
“…Beryllium is challenging to use in fabricating optical elements for several reasons. First, the material can be toxic if small particles enter the airways, which requires extensive safety procedures when being machined [120]. Further, material removal rates are low, surface pitting is precarious, and the material is stress-sensitive even for typical process stresses.…”
Section: 2a Primary Mirror Surfacesmentioning
confidence: 99%
“…This metrology tool guided the fabrication from 25 to 12 μm loose abrasive grinding, which resulted in a 1 μm RMS surface[122]. After the surface reaches this level of roughness, a clear reflection is obtained by a minimal polishing-out run and other more traditional test methods may be used in conjunction with finer fabrication methods.The JWST primary mirror segments were measured during the generation stage using a coordinate measuring machine for initial qualification, providing a spatial resolution of 0.25 mm with an accuracy of 0.3 μm[120]. As the grinding progressed to the point of obtaining a 10 μm RMS roughness, an infrared scanning Shack Hartmann system (SSHS) was employed as a full aperture test.…”
mentioning
confidence: 99%
“…The James Webb Space Telescope (JWST), the successor of the Hubble Space Telescope, is made up of a primary mirror containing 18 segments. Its entrance pupil diameter is 6.6m and its global radius of curvature (GROC) is 15.8m whereas the segment-to-segment radius difference is required to be ±0.1 mm [1] . In our previous research, we suggested the tolerance on radius mismatch was very stringent, and a method of independent radius of curvature (ROC) control was proposed for the individual segments [2] .…”
Section: Introductionmentioning
confidence: 99%
“…In order to reduce the wavefront error close to zero, because the local control method can only change the sag of the center area of each segment, we need to push the wavefront in the outer area to zero and use the coef of the local control to compensate the center area. Therefore, the equation (9) is used to replace the equation(6) in the fourth level compensation and the coef compensation is approximated by Equation (10):1 1…”
mentioning
confidence: 99%