Progress on the realisation of high-resolution thin monolithic shells

M. Civitani, S. Basso, V. Cotroneo, M. Demmer, M. Ghigo, S. Incorvaia, L. Lessio, G. Pareschi, G. Parodi, E. Redaelli, S. Schuler, D. Spiga, G. Toso, G. Vecchi
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引用次数: 1

Abstract

An X-ray Observatory, with superb imaging capabilities and with large throughput, has been recognised as a strategic missions in the Astro2020 decadal survey. The traditional solution foreseen for the realisation of very large x-ray mirror modules (diameters above 1 m) is the partition of the optics in azimuthal and radial modules (like Silicon Pore Optics in Athena). Even if this approach solves the initial problem of the procurement and the handling of very large substrates, it moves the difficulties in the second phase, when thousands of segments have to be assembled without degrading their optical performances. On the contrary, a simpler large mirror module design could correspond to less than a few hundred thin monolithic shells. As an example, the complete opto-mechanical design, compliant with the Lynx mass budget and based on fused silica, foresees that the shell thickness ranges between 2 and 4 mm (for mirror shells between 0.4 and 3 m diameter). The conceptual design of such an mirror module could be refined for smaller scale mission, keeping both the advantage of the design simplicity and of the high-resolution capability, achievable through the direct polishing approach. A technology development roadmap for this approach is funded in Italy by ASI and led by INAF-OAB. In this paper, we present the advancements obtained in the development of the different phases of the process and in the realisation of two new single-reflection shells (SR shells), almost representative of the final optical configuration foreseen for the mirror assembly. The first shell will be used to prove the figuring process in a lab-mount, built upon elements of the previous supporting structure concept. The second shell will be hosted in an upgraded lab-mount structure, which guarantees better performances (frequencies, gravity and thermo-elastic response) and which is suitable to test the transfer of the shell to a spider-like configuration.
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高分辨率薄单片壳的实现进展
具有卓越成像能力和大通量的x射线天文台已被认定为Astro2020年十年调查的战略任务。实现超大x射线反射镜模块(直径超过1米)的传统解决方案是在方位角和径向模块中划分光学元件(如雅典娜的硅孔光学)。即使这种方法解决了最初的采购和处理非常大的基板的问题,它也解决了第二阶段的困难,当成千上万的片段必须在不降低其光学性能的情况下组装时。相反,一个更简单的大型镜像模块设计可以对应不到几百个薄的单片外壳。例如,完整的光学机械设计,符合Lynx质量预算,基于熔融二氧化硅,预计外壳厚度在2到4毫米之间(镜面壳直径在0.4到3米之间)。这种镜像模块的概念设计可以为更小规模的任务进行改进,同时保持设计简单和高分辨率能力的优势,通过直接抛光方法可以实现。该方法的技术开发路线图由ASI在意大利资助,由INAF-OAB领导。在本文中,我们介绍了在该过程的不同阶段的发展和两个新的单反射壳(SR壳)的实现中取得的进展,几乎代表了为镜子组件预见的最终光学配置。第一个外壳将用于在实验室安装中证明计算过程,建立在先前支持结构概念的元素之上。第二个壳将被安置在一个升级的实验室安装结构中,它保证了更好的性能(频率、重力和热弹性响应),并且适合测试壳向蜘蛛状结构的转移。
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