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                    Microtechnologies for Science Instrumentation Applications      135


                    Space Agency (ESA) will be providing the NIRSpec instrument, and NASA will
                    provide the detectors and the MEMS aperture mask as part of their contribution to
                    JWST. Two approaches were initially proposed in 1996 to NASA for the NIRSpec,
                    one using a MEMS micromirror array 36,37  and one using a MEMS shutter array. 31–
                    34
                      The requirements for both mirror and shutter arrays are very strict: The size of
                    each pixel was to be 100   100 mm, with a fill factor better than 80% and a contrast
                    better than 2000:1, expandable to an array size of 1800   1800 square elements,
                    operating at 40K. Two mirror microarray technologies were considered, one devel-
                    oped at NASA GSFC  38  and one at Sandia National Laboratories (SNL). 39
                    A scanning electron microscope (SEM) photograph of the SNL micromirrors is
                    shown in Figure 7.6. The mirrors are made using SNL’s SUMMiT V process as seen
                    in Chapter 3. An advantage of the mirror design is that the drive and selection
                    electronics can be hidden under the mirrors. However, in order to improve the
                    image quality and the contrast, the mirror needs to be fabricated with different
                    materials, gold on silicon in this case, which causes stress when cooled down to
                    cryogenic temperatures. This results in required distortion of the image quality and
                    may cause de-lamination of the gold coating itself.
                       The shutter approach was selected because of its better contrast and image
                    quality, since no reflective surface is involved, and scattered light from the edges is
                    predominantly reflected back away from the spectrograph. A major challenge for
                    this approach is to integrate the actuation mechanism as well as the single shutter
                    control — each shutter needs to be uniquely addressed — within less than 20% of
                    the entire area. The JWST ‘‘microshutter array’’ is a programmable aperture which




























                    FIGURE 7.6 A micromirror developed by SNL, pictured in the tilted position. Each mirror is
                                     1
                    about 100 mm in width. (Courtesy of Sandia National Laboratories, http://www.sandia.gov/
                    media/NewsRel/NR1999/space.htm.)




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