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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伦琴测量)是SRG(Spektrum Rontgen Gamma)任务的主要科学有效载荷,该任务计划于2019年3月发射。其目的地是拉格朗日L2点,其任务是进行一次X射线天空的勘测。 eROSITA是一种复杂的仪器,由七个相同的同心X射线望远镜组成,焦距为1600mm,孔径为7×350mm。每个望远镜都配备有独立的CCD摄像机。冷冗余ITC管理着所有七个摄像机以及望远镜的热控制以及与航天器的接口。该系统的复杂性在于,与航天器的硬件和软件接口最少。在这方面,ITC在仪器管理以及科学数据管理中起着关键作用。就仪器灵活性而言,这被证明是最佳解决方案,但同时也带来了一些挑战。本文概述了eROSITA系统的功能,其接口和操作模式,并概述了在集成和验证整个系统过程中面临的主要挑战。在代表性的热控制条件下,在真空中进行了广泛的端到端测试,验证了该仪器的功能,以验证该仪器在最坏情况下的功能。当前,测试是与航天器结合执行的,以验证eROSITA与航天器之间的通信以及通过俄罗斯无线电联合体(TM / TC系统)进行的数据传输。这包括所有操作和生存模式。本文总结了仪器级和航天器级功能测试的主要结果。

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