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Impact ofionizing radiations on ZERODUR®

机译:电离辐射对ZERODUR®的影响

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摘要

Satellites operating on LEO and GEO trajectories are subject to the effect of ionizing space radiations, mostly electrons, that are concentrated in the Van Allen belts These ionizing radiations are responsible for accelerated ageing (especially compaction, i.e. local material density variation), which is thought to be detrimental for the optical figure of the embedded optical devices. The studies made on this topic during the last four decades, are proposing very different phenomenological power laws description of this effect. However, the simulated deformations derived from these laws are in partial disagreement with the observations made at the laboratory, moreover they do not account for the absence of problems reported during the space missions embedding ZERODUR® material. In order to elucidate these mismatches, we defined a new experimental approach suited for the description of the compaction phenomenon for doses corresponding to typical astrospace missions. An overview of the preparatory simulation work for the design of the irradiation environment, for the design of the build-up shielding material as well as of the design of the target samples will be presented. This study will also give a short description of the experimental irradiations sequence as well as the high precision metrological approaches used in order to determine the changes induced in the ZERODUR®.
机译:在LEO和GEO轨道上运行的卫星受到集中在Van Allen带中的电离空间辐射(主要是电子)的影响。这些电离辐射导致加速老化(特别是压实,即局部材料密度变化),这被认为是对嵌入式光学设备的光学形状有害。在过去的四十年中,关于该主题的研究提出了关于这种效应的非常不同的现象学幂律描述。但是,从这些定律得出的模拟变形与实验室观察到的结果有些不同,而且它们不能说明在太空任务中没有嵌入ZERODUR®材料的问题。为了阐明这些失配,我们定义了一种新的实验方法,适合描述与典型航天任务相对应的剂量的压实现象。将概述用于辐照环境的设计,用于堆积的屏蔽材料的设计以及目标样品的设计的准备模拟工作的概述。这项研究还将简要介绍实验照射顺序以及用于确定ZERODUR®引起的变化的高精度计量方法。

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