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Next-generation hollow retroreflectors for lunar laser ranging

机译:用于月球激光测距的下一代空心后向反射器

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The three retroreflector arrays put on the Moon 40 years ago by the Apollo astronauts and the French-built arrays on the Soviet Lunokhod rovers continue to be useful targets, and have provided the most stringent tests of the Strong Equivalence Principle and the time variation of Newton's gravitational constant, as well as valuable insight into the Moon's interior. However, the precision of the ranging measurements are now being limited by the physical size of the arrays and a new generation of retroreflectors is required to make significant advances over current capabilities. Large single-cube retroreflectors represent the most promising approach to overcoming current limitations, and hollow retroreflectors in particular have the potential to maintain their good optical performance over the nearly 300 K temperature swing that occurs during the lunar cycle. Typically, epoxies are used for aligning and bonding hollow retroreflectors, but their thermal stability will predominantly be limited by the difference of the coefficient of thermal expansion (CTE) between the epoxy and the glass. A relatively new bonding method known as hydroxide catalysis bonding (HCB) has been used to adhere complex optical components for space-based missions. HCB has an extremely thin bond, a low CTE, and a high breaking strength that makes it an ideal candidate for bonding hollow retroreflectors for lunar laser ranging (LLR). In this work, we present results of a feasibility study of bonded Pyrex and fused silica hollow retroreflectors using both epoxy and HCB methods, including the results of thermally cycling the hollow retroreflectors from 295 to 185 K. Finally, we discuss the potential for using these retroreflectors for future LLR.
机译:40年前,由阿波罗宇航员在月球上放置的三个后向反射器阵列和在苏联Lunokhod漫游车上的法国制造的阵列仍然是有用的目标,并且提供了对强当量原理和牛顿星时差的最严格测试引力常数,以及对月球内部的宝贵见识。但是,测距测量的精度现在受到阵列的物理尺寸的限制,并且需要新一代的后向反射器才能在当前性能上取得重大进步。大型单立方逆反射器是克服电流限制的最有前途的方法,特别是中空逆反射器有可能在月球周期发生的近300 K的温度波动中保持其良好的光学性能。通常,环氧树脂用于对准和粘结中空的后向反射器,但是它们的热稳定性将主要受到环氧树脂和玻璃之间热膨胀系数(CTE)的差异的限制。被称为氢氧化物催化键合(HCB)的一种相对较新的键合方法已被用于粘附复杂的光学组件以进行基于太空的飞行任务。 HCB具有极薄的键合,低的CTE和高的断裂强度,使其成为月球激光测距(LLR)的空心后向反射镜的理想选择。在这项工作中,我们介绍了使用环氧树脂和HCB方法对粘合的派热克斯和熔融石英空心后向反射镜进行可行性研究的结果,包括将空心后向反射镜从295 K循环到185 K的热循环的结果。最后,我们讨论了使用这些材料的潜力未来LLR的后向反射器。

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