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eROSITA System Functionality and Operation

机译:erosita系统功能和操作

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eROSITA (extended ROentgen Survey with an Imaging Telescope Array) is the primary scientific payload on board the SRG (Spektrum Rontgen Gamma) mission, scheduled for launch in March 2019. Its destination is the Lagrangian point L2, and its mission is to make a full survey of the X-ray sky. eROSITA is a complex instrument composed of seven identical co-aligned X-ray telescopes with a focal length of 1600mm and an aperture of 7×350mm. Each telescope is equipped with an independent CCD camera. The cold redundant ITC manages all seven cameras as well as the thermal control of the telescope and the interface to the spacecraft. The complexity of this system resides in the fact that the hardware and software interfaces to the spacecraft are minimal. In this respect the ITC has a key role in the management of the instrument, as well as in the science data management. This proved to be an optimal solution in terms of instrument flexibility, but also presented some challenges. The paper presents an overview on the eROSITA system functionality, its interfaces and operational modes together with an outline of the main challenges, which were faced during integration and verification of the complete system. The function of the instrument was verified in the frame of an extensive end-to-end test in vacuum under representative thermal control conditions to verify that the instrument functions under worst case conditions. Currently tests are performed in combination with the spacecraft to verify communication between eROSITA and the spacecraft and the data transfer through the Russian radio complex (TM/TC system). This includes all operational and survival modes. The paper summarizes the main results of the functional tests on instrument level and on spacecraft level.
机译:Erosita(带有成像望远镜阵列的扩展Roentgen调查)是SRG(Spektrum Rontgen Gamma)使命的主要科学有效载荷,计划于2019年3月推出。其目的地是拉格朗日点L2,其使命是完整X射线天空的调查。 Erosita是由七个相同的共控制X射线望远镜组成的复杂仪器,其焦距为1600mm,孔径为7×350mm。每个望远镜都配有独立的CCD相机。冷冗余ITC管理所有七个摄像机以及望远镜的热控制和航天器的界面。该系统的复杂性驻留在于对航天器的硬件和软件接口很小。在这方面,ITC在仪器管理中具有关键作用,以及科学数据管理。这被证明是在仪器灵活方面是最佳解决方案,但也呈现出一些挑战。本文概述了伊斯罗伊系统功能,其接口和操作模式以及主要挑战的概要,在整合和验证完整系统期间面临的主要挑战。在代表性热控制条件下,在真空中的广泛端到端测试框架中验证了仪器的功能,以验证仪器在最坏情况下功能。目前测试与航天器相结合进行,以验证伊罗地图和航天器之间的通信以及通过俄罗斯无线电复合体(TM / TC系统)的数据传输。这包括所有操作和生存模式。本文总结了仪器水平和航天器水平功能测试的主要结果。

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