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Space radiation environment effects on X-ray CCD background

机译:空间辐射环境对X射线CCD背景的影响

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Charge coupled devices (CCDs) are often employed as the detector of choice for observing X-rays in space. The instrument background experienced in orbit has a major impact on the overall sensitivity of the camera system. The instrument background for the European Space Agency X-ray Multi Mirror (XMM-Newton) mission was found to be much greater in orbit than that originally predicted pre-launch, the reasons for which still being up for discussion. The Geant4 toolkit provides a framework for Monte Carlo simulations in a variety of areas in science and is used here to simulate the instrument background for several CCD based detectors in-orbit in order to gain a further insight into the formation of the instrument background continuum. The missions discussed in this paper include the ESA XMM-Newton mission, the NASA Swift mission and the Japanese Space Agency Suzaku mission. These three missions allow a comparison between the effects of both the mission orbit and the detector construction on the instrument background count-rate. Analysis of the results from the simulation lead to the conclusion that knock-on electrons, produced when protons pass through the shielding, dominate the instrument background continuum at the XMM-Newton Highly Elliptical Orbit (HEO) with a perigee and apogee of approximately 7000 and 120 000 km respectively, forming an additional background component not considered in the pre-launch study. The surface properties of the detector and shielding have the greatest impact on the level of the instrument background due to the interaction length of the knock-on electrons produced. At the Low Earth Orbit (LEO) of Swift and Suzaku at approximately 600 km, the impact of the knock-on electrons is reduced due to the differing in-flux of protons, and the form of the instrument background can vary greatly with the detector construction. The inconsistencies between this study and the pre-launch simulations are discussed. Sensitivity considerations regarding the instrument background are deliberated with a view towards future missions.
机译:电荷耦合器件(CCD)通常用作观察空间X射线的首选检测器。在轨道上经历的仪器背景对摄像机系统的整体灵敏度有重大影响。发现欧洲航天局X射线多镜(XMM-Newton)任务的仪器背景在轨道上比最初预测的发射前要大得多,其原因尚待讨论。 Geant4工具包为科学的各个领域提供了蒙特卡洛模拟的框架,并在此处用于模拟多个在轨的基于CCD的探测器的仪器背景,以进一步了解仪器背景连续体的形成。本文讨论的任务包括ESA XMM-牛顿任务,NASA迅速任务和日本航天局朱雀任务。这三个任务可以比较任务轨道和探测器构造对仪器本底计数率的影响。对模拟结果的分析得出的结论是,质子穿过屏蔽层时产生的敲击电子在XMM-牛顿高椭圆轨道(HEO)的仪器本底连续体中占主导地位,其近地点和远地点约为7000和分别达到12万公里,这构成了发射前研究中未考虑的其他背景要素。由于产生的敲击电子的相互作用长度,检测器和屏蔽的表面特性对仪器本底水平的影响最大。在斯威夫特和朱雀的低地球轨道(LEO)约600公里处,由于质子的流入量不同,撞击电子的影响减小了,并且仪器背景的形式会随探测器的不同而变化很大施工。讨论了这项研究与启动前模拟之间的不一致之处。考虑到仪器背景的敏感性考虑因素,以应对未来的任务。

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