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                   166                       MEMS and Microstructures in Aerospace Applications


                       Either electrostatic or electromagnetic drive mechanisms can be used to move
                   the mirrors, but electrostatic is preferred, since it takes up little room and needs
                   relatively low power. Large switch sizes, using relatively large mirrors (approxi-
                   mately few millimeters) with long focal lengths (tens of centimeters) are desired to
                   allow the use of larger light beams, which have less beam divergence and greater
                   useful relay distances. Larger angular deflections are also desirable.

                   8.6.2 PERFORMANCE REQUIREMENTS
                   Recent collaborative work between MEMX Corporation and the Johns Hopkins
                   University Applied Physics Laboratory (JHU/APL) 107  has focused on developing
                   MEMS micromirror technology for free-space multiaccess optical communications
                   between spacecraft. Key performance issues addressed in this effort for space-based
                   optical communications include micromirror heating due to input laser power,
                   achievable degree of mechanical damping at ambient and partial air pressures,
                   micromirror flatness, element size, angular field-of-regard (FOR), control-loop
                   bandwidth, and open-loop transfer function shape. For some parameters, these
                   devices already meet the ‘‘desired’’ application requirements, and for all cases,
                   experimental tests indicate that the application requirements can be met with some
                   redesign of existing devices. For example, the MEMX devices measured angular
                   field-of-regard (FOR) was approximately +7.98 optical, but would need to be +128
                   for a projected redesign for GEO-to-ground links, which is quite feasible with
                   slight micromirror redesign. Measured angular resolution was less than 360 mrad
                   (desired greater than 1000 mrad); bandwidth was approximately 1 kHz (desired 100
                   to 1000 Hz); and mirror radius of curvature was approximately 0.4 m (nominally
                   0.5 m approximately). These and other key device parameters (and their desired
                   range of values) are given in Table 8.1.







                           TABLE 8.1
                           Device Parameters of MEMX Micromirrors
                           Parameter                               Nominal Value

                           Angular field-of-regard               +128 (+210 Vmrad) a
                           Angular resolution                    1 mrad a
                           Closed-loop bandwidth                 100 to 1000 Hz
                           Number of elements                    4   4 (minimum)
                           Element size                          0.5 mm
                           Element pitch                         ~2 mm
                           Element radius of curvature           ~0.5 m
                           Angle or voltage scale factor         10 mrad/mV
                           a
                           Before beam expansion.





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