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Laser beaming demonstrations to high-orbit satellites

机译:对高轨道卫星的激光束演示

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Abstract: A team of Phillips Laboratory, COMSAT Laboratories, andSandia National Laboratories plans to demonstratestate-of-the-art laser-beaming demonstrations tohigh-orbit satellites. The demonstrations will utilizethe 1.5-m diameter telescope with adaptive optics atthe AFPL Starfire Optical Range (SOR) and a ruby laserprovided by the Air Force and Sandia (1 - 50 kW and 6ms at 694.3 nm). The first targets will be corner-cuberetro-reflectors left on the moon by the Apollo 11, 14,and 15 landings. We attempt to use adaptive optics foratmospheric compensation to demonstrate accurate andreliable beam projection with a series of shots over aspan of time and shot angle. We utilize the returnsignal from the retro- reflectors to help determine thebeam diameter on the moon and the variations inpointing accuracy caused by atmospheric tilt. This isespecially challenging because the retro-reflectorsneed to be in the lunar shadow to allow detection overbackground light. If the results from this experimentare encouraging, we will at a later date direct thebeam at a COMSAT satellite in geosynchronous orbit asit goes into the shadow of the earth. We utilize anonboard monitor to measure the current generated in thesolar panels on the satellite while the beam ispresent. A threshold irradiance of about 4 W/m$+2$/ onorbit is needed for this demonstration. !11
机译:摘要:菲利普斯实验室,COMSAT实验室和Sandia国家实验室的团队计划向高轨道卫星演示最新的激光束演示。演示将利用直径为1.5 m的望远镜和AFPL星火光学范围(SOR)上的自适应光学系统以及空军和桑迪亚提供的红宝石激光器(1-50 kW和694.3 nm处的6毫秒)。第一个目标将是阿波罗11号,14号和15号着陆点留在月球上的弯角立方反射镜。我们尝试使用自适应光学大气压补偿技术来演示准确和可靠的光束投影,以及在时间和拍摄角度上的一系列拍摄。我们利用后向反射器的返回信号来帮助确定月球上的光束直径以及由大气倾斜引起的指向精度变化。这尤其具有挑战性,因为后向反射器必须位于月球阴影中才能检测背景光。如果该实验的结果令人鼓舞,我们稍后将在地球同步进入地球同步轨道时,将光束对准地球同步轨道上的COMSAT卫星。当光束出现时,我们利用机载监视器测量卫星太阳能板上产生的电流。该演示需要约4 W / m $ + 2 $ /在轨辐射强度的阈值。 !11

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