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Slumped glass option for making the XEUS mirrors: preliminarydesign and ongoing developments

机译:玻璃镜选择的玻璃选项:预先设计和正在进行的发展

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The XEUS mission (X-ray Evolving-Universe Spectroscopy Mission) of ESA, in the present configuration has a mirror collecting area in the order of 5-6 m~2 @ 1 keV, 2 m~2 @ 7 keV and 1 m~2 @ 10 keV. These large collecting areas could be obtained with a mirror assembly composed of a large number of high quality segments each being able to deliver the angular resolution requested by the mission or better. The XEUS telescope will fit in the fairing of an Ariane 5 ECA launcher and hence its diameter is presently of about 4.5 m. The request in terms of angular resolution of the telescope has been set to 5 arcsec with a goal of 2 arcsec. Due to the large size of the optics it is impossible to create closed shells like those used for XMM or Chandra and hence it will be necessary to assemble a large number of segments (for example of –0.6 m x –0.3 m size) to recreate the mirror shells. These segments will form a module, an optical sub-unit of the telescope. The modules will be assembled to form the whole mirror system. As for all the space missions, the limits imposed on the payload mass budget by the launcher is the main driver that force the use of very lightweight optics and this request is of course very challenging. For example, the current design for XEUS foresees a geometric-area/mass ratio better than about 30 cm2/kg. In this article is illustrated a possible approach for the realization of large size and lightweight X-ray mirrors that derive from an experience gained from a previous work made in INAF-OAB on the thermal slumping of thin glass optics. The process foresees the use of a mould having a good optical figure but opposite shape respect to the segment to be slumped. On the mould is placed an initially flat glass sheet. With a suitable thermal cycle the glass sheet is conformed to the mould shape. Once tested for acceptance the glass sheet it is then integrated into a module by means of a robotic arm having a feedback system to confirm the correct alignment. A study on different optical geometries using the classical Wolter I and Kirkpatrick-Baez configurations has been also performed to investigate the theoretical performances obtainable with optics made using very thin glass shells.
机译:ESA的Xeus Mission(X射线演化 - 宇宙谱任务),在本配置中具有镜子收集面积,大约为5-6 m〜2 @ 1kev,2 m〜2 @ 7kev和1 m〜 2 @ 10 kev。可以通过由大量高质量段组成的镜子组件来获得这些大收集区域,每个镜子组成每个能够提供任务或更好的角度分辨率。 Xeus望远镜将适合Ariane 5 ECA发射器的整流罩,因此其直径目前约为4.5米。在望远镜的角度分辨率方面的请求已设置为5个arcsec,其目标为2个arcsec。由于光学尺寸的大尺寸,不可能创建像XMM或Chandra那些一样的封闭壳,因此需要组装大量的段(例如-0.6 mx -0.3 m尺寸)来重新创建镜子壳。这些段将形成模块,望远镜的光学子单元。模块将组装以形成整个镜像系统。至于所有空间任务,发射器对有效载荷质量预算的限制是强制使用非常轻量级光学器件的主要驱动因素,此请求当然非常具有挑战性。例如,Xeus的当前设计预示着几何区域/质量比优于约30cm2 / kg。在本文中,示出了实现大尺寸和轻质X射线镜的可能方法,该X射线镜得出从在薄型玻璃光学器件的热坍塌上从INAF-OAB中进行的先前工作中获得的经验。该过程预见使用具有良好光学图形的模具,而是相对于待坍塌的段的形状。在模具上放置初始平坦的玻璃板。具有合适的热循环,玻璃板符合模具形状。一旦测试接受玻璃板,然后通过具有反馈系统的机器人臂集成到模块中以确认正确的对准。还研究了使用经典沃尔特I和KIRKPATRICK-BAEZ配置的不同光学几何图中的研究,以研究使用非常薄的玻璃壳制造的光学器件可获得的理论性能。

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