SVOM飞行模型龙虾眼光学的标定

C. Feldman, R. Willingale, J. Pearson, G. Butcher, Philip Peterson, T. Crawford, P. Houghton, R. Speight, A. Lodge, C. Bicknell, J. Osborne, P. O'Brien, M. Bradshaw, V. Burwitz, G. Hartner, A. Langmeier, T. Müller, S. Rukdee, Thomas Schmidt, D. Götz, K. Mercier, J. Le Duigou, F. Gonzalez, E. Schyns, Romain Roudot, R. Fairbend, J. Séguy
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引用次数: 4

摘要

天基多波段天文可变物体监测仪(SVOM)是一项中法合作的任务,将于2023年发射。它由四个空间仪器组成:ECLAIRs,用于探测x射线和伽马射线瞬变;GRM,伽马射线光谱仪;VT,可见光望远镜和微通道x射线望远镜(MXT)。MXT的主要目标是精确定位和光谱表征伽马射线爆发后的x射线余辉。MXT是一种窄视场优化的龙虾眼x射线聚焦望远镜,由25个方形微孔光学(mpo)阵列组成,具有1平方度的探测器限制视场,工作在0.2-10 keV的能量带。SVOM飞行模型(FM) MXT光学(MOP)在莱斯特大学设计、建造和初步测试,MOP的全面校准在PANTER设施(MPE)完成。然后将其集成到完整的原型飞行模型(PFM) MXT仪器中,然后返回PANTER进行PFM MXT的完整校准。我们将光学性能作为FM MXT仪器校准的一部分。研究了从C-K (0.28 keV)到Ge-K (9.89 keV) 11种能量下望远镜的响应,包括测量了有效面积和PSF的大小和形状。确定了仪器的焦距,并介绍了用于预测性能的建模和分析的细节。实测结果表明,实际有效面积和PSF与模型吻合较好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Calibration of the flight model lobster eye optic for SVOM
The space-based multi-band astronomical variable objects monitor (SVOM) is a Chinese–French mission due to be launched in 2023. It is composed of four space borne instruments: ECLAIRs, for detecting x-ray and gamma-ray transients; GRM, a gamma-ray spectrometer; VT, a visible telescope and the Microchannel X-ray Telescope (MXT). The MXT’s main goal is to precisely localize, and spectrally characterize x-ray afterglows of gamma-ray bursts. The MXT is a narrow-field-optimised lobster eye x-ray focusing telescope comprising an array of 25 square micro pore optics (MPOs), with a detector-limited field of view of ∼1 square degree, working in the energy band 0.2-10 keV. The SVOM flight model (FM) MXT optic (MOP) was designed, built and initially tested at the University of Leicester and a full calibration of the MOP was completed at the PANTER facility (MPE). It was then integrated in to the full proto flight model (PFM) MXT instrument before it returned to PANTER for the PFM MXT’s full calibration. We present the optic performance as part of the full FM MXT instrument calibration. The response of the telescope was studied at 11 energies from C-K (0.28 keV) to Ge-K (9.89 keV), including measurements of the effective area and the PSF size and shape. The focal length of the instrument was determined and details of the modelling and analysis used to predict the performance are presented. The measurements demonstrate that the actual effective area and PSF are in good agreement with the modelling.
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