用于减缓银河宇宙射线和太阳粒子事件的氢和甲烷负载屏蔽材料

K. Rojdev, W. Atwell
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引用次数: 2

摘要

深空恶劣的辐射环境是人类航天飞行面临的挑战之一。目前减轻辐射的最佳做法是通过设计和多功能材料。多年来有许多研究表明,低z材料是太空飞行中最好的辐射减缓剂。此外,最近也有一些关于燃料电池材料的氢负载的研究。如果有可能在材料中加入额外的低z材料(如氢),就有可能增加这些材料的辐射缓解潜力。因此,我们的工作重点是金属氢化物(mh)、金属有机框架(mof)和纳米多孔碳复合材料(CNTs),它们可以装载氢或甲烷以减缓辐射。我们之前的模拟工作只关注氢负载,并研究了这些材料在1989年10月的一次特别硬的太阳粒子事件(SPE)中的性能。在这些模拟中,我们发现50%的碳复合材料的性能优于高密度聚乙烯(HDPE)——目前被动辐射屏蔽的标准。我们还发现10%的mof的性能优于HDPE。因此,我们希望继续对这些材料进行模拟研究,以确定它们在银河宇宙射线(GCR)环境中是否也比HDPE表现出改善。此外,由于氢气的可燃性和在极端温度下的不稳定性,使用氢气作为装载材料也存在一些问题。因此,我们也在考虑mof和CNTs的甲烷负载。本文将对这项工作的细节进行讨论。总体而言,与我们的典型航天器材料铝和标准屏蔽材料HDPE相比,结果表明几种mof、CNTs和mh的性能非常好。本研究还表明,相同碱化学性质的载氢材料和载甲烷材料在剂量上差别不大。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Hydrogen- and Methane-Loaded Shielding Materials for Mitigation of Galactic Cosmic Rays and Solar Particle Events
ABSTRACT One of the challenges of human spaceflight in deep space is the harsh radiation environment. The current best practices for mitigating radiation are via design and multifunctional materials. There have been many studies over the years showing low-Z materials as the best radiation mitigators for spaceflight. In addition, there have recently been several studies investigating hydrogen-loading of materials for fuel cells. If it is possible to load a material with additional low-Z materials — such as hydrogen — it may be possible to increase the radiation mitigating potential of these materials. Thus, our work is focused on metal hydrides (MHs), metal organic frameworks (MOFs), and nanoporous carbon composites (CNTs) that can be loaded with hydrogen or methane for radiation mitigation. Our previous simulation work focused on hydrogen-loading only, and investigated the capability of these materials during a particularly hard solar particle event (SPE) in October 1989. In these simulations, we found 50% of the investigated carbon composites outperformed high-density polyethylene (HDPE) — the current standard for passive radiation shielding. We also found 10% of the investigated MOFs outperformed HDPE. Therefore, we wanted to continue our simulation study of these materials to determine whether they may also show improvement over HDPE in a galactic cosmic ray (GCR) environment. Furthermore, there are concerns with using hydrogen as a loading material — a result of its flammability and instability in thermal extremes. Thus, we are also considering methane-loading of the MOFs and CNTs. The details of this work will be discussed in the paper. Overall, the results showed several MOFs, CNTs, and MHs that performed very well when compared with our typical spacecraft material of aluminum and our standard shielding material of HDPE. This study also showed there is little difference in the dose between hydrogen-loaded and methane-loaded materials of the same base chemistry.
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