eXTP光学元件结构的设计与测试

Z. Song, J. Ma, J. Wang, A. Zhang, Y. Wang, Y. J. Yang, W. Jiang, Y. Chen, K. Yu, S. Yang, Y. Xu, H. He, F. Lu, S. Zhang, S. Basso, M. Civitani, G. Pareschi, G. Sironi, D. Spiga, V. Cotroneo, G. Tagliaferri, L. Sheng, Y. Q. Yan, P. Qiang, B. Zhao
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引用次数: 0

摘要

缩写“eXTP”代表增强x射线定时和偏振测量,这是中国科学家发起的一项重点科学任务,旨在研究物质在密度、重力和磁性极端条件下的状态[1]。各种有效载荷将在卫星上。SFA,即光谱聚焦阵列,由九个相同的x射线望远镜组成,工作在0.5-10 keV的能量范围内,将是这里的焦点[1]。每台SFA的视场为12 arcmin,在2 keV和6 keV下,每台SFA的采集面积分别为900 cm2和550 cm2[1]。本文首先简要介绍了一般光学,然后介绍了一些重要的设计方面。它涵盖了从结构和热设计到CAE分析以及现状的内容。大口径、大焦距的光学元件在发射装置给定的恶劣条件下,必然会给承载结构的鲁棒性带来大问题。根据目前的设计,镜子组件将有3英尺和24条辐条。IHEP已经对一些原型机进行了振动试验,并对设计的可行性进行了初步评估。它清楚地表明,目前的设计只有一个蜘蛛可能通过振动测试,假设一个折衷的测试条件。随后调整CAE模型以匹配测试结果,可用于不久的将来的进一步评估。当然,我们的争论总是存在不确定性。更详细的原型和机械上完全具有代表性的炮弹仍在设计中。希望能尽快获得高度可靠的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and testing of the structure of the eXTP optics
The abbreviation “eXTP” represents the enhanced x-ray timing and polarimetry, which is a key science mission initiated by the Chinese scientists, designed to study the state of matter under extreme conditions of density, gravity and magnetism [1]. Various payloads would be on board of the satellite. The SFA, namely the spectroscopy focusing array, consisting of nine identical x-ray telescopes working in the energy range of 0.5-10 keV, will be the focus here [1]. SFA has a field-of-view of 12 arcmin for each and a collecting area of 900 cm2 and 550 cm2 for each at 2 keV and 6 keV respectively [1]. This paper starts with a brief introduction of the general optics, and then goes across some important design aspects. It covers contents from the structural and thermal designs to the CAE analyses as well as the current status. The large diameter and huge focal length of the optics will definitely bring big issues to the robustness of the carrying structure under the severe conditions given by the launcher. According to the current design, the mirror assembly will have 3 feet and 24 spokes. Vibration tests were already performed on a few prototypes by IHEP, and a preliminary evaluation on the feasibility of the design has been achieved. It clearly stated that the current design with only a single spider can probably survive the vibration tests assuming a compromised test condition somewhere. CAE models were adjusted thereafter to match the test results, which could be used for further assessments in a near future. Of course, there are always uncertainties associated with our arguments. More detailed prototypes with mechanically fully representative shells were still under design. Hopefully, highly reliable results could be retrieved soon.
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