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                    Microelectromechanical Systems for Spacecraft Communications    169


                    disposed 1208 apart around the periphery. Each leg is 0.9 mm long and is actuated
                    by a linear electrostatic comb drive. To elevate the mirror in a piston motion to a
                    nominal elevation of 50 mm for subsequent tip or tilt actuation, a voltage of 30 V
                    must be applied to each leg. To cause a tip deflection, legs 2 and 3 can be held
                    stationary while leg 1 is actuated with an appropriate (e.g., sine wave) drive signal
                    with nominal peak amplitude of 50 V. To cause a tilt deflection, legs 2 and 3 can be
                    driven 1808 out-of-phase with each other while leg 1 is held stationary. Greater
                    dynamic range can be achieved for the tip-case by actuating opposing legs as in the
                    tilt case. Several test articles of this type were evaluated.
                       The MEMX micromirrors assessed were manufactured using polysilicon sur-
                    face machining technology developed at Sandia National Laboratory; however, this
                    technology has since been transferred to Fairchild Semiconductor in Portland,
                    Maine.


                    8.7 APPLICATIONS OF MEMS TO SPACECRAFT
                         OPTICAL COMMUNICATIONS
                    Optical communication links offer many advantages over microwave links. In
                    particular, free-space laser systems can provide narrow beam widths and high
                    gains with much smaller hardware. High gains allow for much higher data rates,
                    on the order of Gbps for sufficiently close link ranges, for example, near terrestrial
                    space. 4
                       The Jet Propulsion Laboratory (JPL) in association with NASA is building an
                    Optical Communications Telescope Laboratory (OCTL) transceiver station at its
                    Table Mountain Facility, and they have explored laser communications links for
                    deep space communications (the Galileo Optical Experiment) and near-terrestrial
                                                                   3
                    communications (Ground Orbit Lasercom Demonstration). More recently the Mars
                    Laser Communications Demonstrator (MLCD) program has begun to develop an
                    optical telecomm terminal for the Mars Telecommunications Orbiter (MTO),
                    scheduled for launch in 2009. 110  Data rates ranging from 1 to 2.5 Gbps are planned
                    for future near-terrestrial space demonstrations and up to 30 Mbps for deep space
                                     3
                    links such as MLCD. Laser downlinks have also been explored for communication
                    with submarines via satellite. 111

                    8.7.1 OPTICAL BEAM STEERING
                    Recent collaborative work between MEMX Corporation and JHU/APL 107  was
                    based on previously developed MEMX optical switches. These special test units
                    were evaluated for applications in laboratory tests as beamsteerers using a digital
                    pointing and tracking system. Highly accurate and stabilized body-mounted track-
                    ing systems are essential to the implementation of long-haul optical communication
                    channels and could be operated potentially from geosynchronous earth orbit (GEO)
                    to ground-based or air-platform optical receiver terminals. For such spacecraft
                    applications, moderate to high-powered laser diodes are likely to be required.
                    Coupled with their potential operation at partial atmospheric pressures, MEMS




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