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美国国家航空航天局马歇尔太空飞行中心的全壳式X射线光学器件研发。

Full-shell x-ray optics development at NASA Marshall Space Flight Center.

作者信息

Kilaru Kiranmayee, Ramsey Brian D, Baumgartner Wayne H, Bongiorno Stephen D, Broadway David M, Champey Patrick R, Davis Jacqueline M, O'Dell Stephen L, Elsner Ronald F, Gaskin Jessica A, Johnson Samantha, Kolodziejczak Jeffery K, Roberts Oliver J, Swartz Douglas A, Weisskopf Martin C

机构信息

Universities Space Research Association, Huntsville, Alabama, United States.

NASA Marshall Space Flight Center, Huntsville, Alabama, United States.

出版信息

J Astron Telesc Instrum Syst. 2019 Apr;5(2). doi: 10.1117/1.jatis.5.2.021010. Epub 2019 Apr 5.

DOI:10.1117/1.jatis.5.2.021010
PMID:32905453
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7473390/
Abstract

NASA's Marshall Space Flight Center (MSFC) maintains an active research program toward the development of high-resolution, lightweight, grazing-incidence x-ray optics to serve the needs of future x-ray astronomy missions such as Lynx. MSFC development efforts include both direct fabrication (diamond turning and deterministic computer-controlled polishing) of mirror shells and replication of mirror shells (from figured, polished mandrels). Both techniques produce full-circumference monolithic (primary + secondary) shells that share the advantages of inherent stability, ease of assembly, and low production cost. However, to achieve high-angular resolution, MSFC is exploring significant technology advances needed to control sources of figure error including fabrication- and coating-induced stresses and mounting-induced distortions.

摘要

美国国家航空航天局马歇尔太空飞行中心(MSFC)正在开展一项积极的研究计划,致力于开发高分辨率、轻质掠入射X射线光学器件,以满足未来诸如“天猫座”等X射线天文学任务的需求。MSFC的研发工作包括镜筒的直接制造(金刚石车削和确定性计算机控制抛光)以及镜筒的复制(从有形状的抛光芯轴复制)。这两种技术都能制造出全圆周整体式(主镜+副镜)镜筒,具有固有稳定性、易于组装和生产成本低等优点。然而,为了实现高角分辨率,MSFC正在探索控制形状误差源所需的重大技术进步,这些误差源包括制造和涂层引起的应力以及安装引起的变形。

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Non-null full field X-ray mirror metrology using SCOTS: a reflection deflectometry approach.使用SCOTS的非零全场X射线镜计量学:一种反射偏转测量方法。
Opt Express. 2012 May 21;20(11):12393-406. doi: 10.1364/OE.20.012393.