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首页> 外文期刊>Plasma Science, IEEE Transactions on >Variations in Cathodoluminescent Intensity of Spacecraft Materials Exposed to Energetic Electron Bombardment
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Variations in Cathodoluminescent Intensity of Spacecraft Materials Exposed to Energetic Electron Bombardment

机译:受到高能电子轰击的航天器材料阴极发光强度的变化

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摘要

Many contemporary spacecraft materials exhibit cathodoluminescence when exposed to electron flux from the space plasma environment. A quantitative physics-based model has been developed to predict the intensity of the total glow as a function of incident electron current density and energy, temperature, and intrinsic material properties. We present a comparative study of the absolute spectral radiance for more than 20 types of dielectric and composite materials based on this model, which spans more than three orders of magnitude. Variations in intensity are contrasted for different electron environments, different sizes of samples and sample sets, different testing and analysis methods, and data acquired at different test facilities. Together, these results allow us to estimate the accuracy and precision to which laboratory studies may be able to determine the response of spacecraft materials in the actual space environment. It also provides guidance as to the distribution of emissions that may be expected for sets of similar flight hardware under similar environmental conditions.
机译:当暴露于来自太空等离子体环境的电子通量时,许多当代航天器材料都显示出阴极发光。已经开发出基于物理的定量模型,以预测总辉光强度与入射电子电流密度,能量,温度和固有材料特性的关系。我们基于此模型对20多种类型的介电和复合材料的绝对光谱辐射率进行了比较研究,该模型跨越了三个数量级。针对不同的电子环境,不同大小的样品和样品组,不同的测试和分析方法以及在不同的测试设施获取的数据,对比了强度变化。综合起来,这些结果使我们能够估计实验室研究能够确定实际空间环境中航天器材料响应的精度和精确度。它还提供了有关在类似环境条件下类似飞行硬件套件可能预期的排放分布的指导。

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