This paper discusses the coarse pointing assembly (CPA) requirements for the optical Multiple Access intersatellite link system. Mechanical and optical design aspects of a periscopic CPA with azimuth and elevation angular ranges of 360 degrees and plus/minus 120 degrees respectively, clear aperture of 7 cm, and a step size of 0.09 degrees are described. Mass budget estimates for a flight unit are presented. The total mass and maximum power consumption are 3.8 kg and 12 W respectively.
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