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Corner-cube retro-reflector instrument for advanced lunar laser ranging

机译:用于高级月球激光测距的角立方复古反射仪

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摘要

Lunar laser ranging (LLR) has made major contributions to our understandingof the Moon's internal structure and the dynamics of the Earth-Moon system.Because of the recent improvements of the ground-based laser rangingfacilities, the present LLR measurement accuracy is limited by theretro-reflectors currently on the lunar surface, which are arrays of smallcorner-cubes. Because of lunar librations, the surfaces of these arrays do not,in general, point directly at the Earth. This effect results in a spread ofarrival times, because each cube that comprises the retroreflector is at aslightly different distance from the Earth, leading to the reduced rangingaccuracy. Thus, a single, wide aperture corner-cube could have a clearadvantage. In addition, after nearly four decades of successful operations theretro-reflectors arrays currently on the Moon started to show performancedegradation; as a result, they yield still useful, but much weaker returnsignals. Thus, fresh and bright instruments on the lunar surface are needed tocontinue precision LLR measurements. We have developed a new retro-reflectordesign to enable advanced LLR operations. It is based on a single, hollowcorner cube with a large aperture for which preliminary thermal, mechanical,and optical design and analysis have been performed. The new instrument will beable to reach an Earth-Moon range precision of 1-mm in a single pulse whilebeing subjected to significant thermal variations present on the lunar surface,and will have low mass to allow robotic deployment. Here we report on ourdesign results and instrument development effort.
机译:月球激光测距(LLR)为我们对月球内部结构和地月亮系统动力学的理解做出了重要贡献。当前在月球表面上的反射器,是小角立方体的阵列。由于月球的释放,这些阵列的表面通常不会直接指向地球。这种影响导致到达时间的扩散,因为组成后向反射器的每个立方体与地球的距离略有不同,从而导致测距精度降低。因此,单个大孔径角锥盒可能具有明显的优势。另外,经过近四十年的成功运作,目前在月球上的反射镜阵列开始表现出性能下降;结果,它们的输出仍然有用,但是返回信号要弱得多。因此,需要使用月球表面上新鲜而明亮的仪器来继续进行精确的LLR测量。我们已经开发了一种新的后向反射器设计,以实现高级LLR操作。它基于具有大孔径的单个空心角立方体,已对其进行了初步的热,机械和光学设计和分析。新仪器将在月球表面受到明显的热变化的情况下,在单个脉冲中达到1毫米的月球范围精度,并且重量轻,可以进行机器人部署。在这里,我们报告我们的设计结果和仪器开发工作。

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