Affiliation:
1. 1 Systems Engineering and Test Branch, NASA Johnson Space Center , Houston, TX United States ;
2. 2 (Retired) Research & Technology, Boeing , Houston, TX United States
Abstract
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.
Reference38 articles.
1. Atwell W (2012) ExtraVehicular (EVA) Operations in the Geostationary Environment. 42nd International Conference on Environmental Systems, AIAA Technical Paper Number 2012-3646
2. Atwell W, Nealy J, Clowdsley M (2006) Space Radiation Exposure Mitigation: Study of Select Materials. International Conference on Environmental Systems, SAE Technical Paper Number 2006-01-2103
3. Atwell W, Rojdev K, Aghara S, Sriprisan S (2013) Mitigating the Effects of the Space Radiation Environment: A Novel Approach of Using Graded-Z Materials. AIAA SPACE 2013 Conference and Exposition, AIAA Technical Paper
4. Atwell W, Rojdev K, Liang D, Hill M (2014) Metal Hydrides, MOFs, and Nanoporous Carbon Composites as Space Radiation Shielding Mitigators. International Conference on Environmental Systems, SAE Technical Paper Number 103
5. Atwell W, Tylka A, Dietrich W, Rojdev K (2010) Band Function Fit to 23rd Solar Cycle Ground Level Proton Events and Radiation Exposure Assessments. 40th International Conference on Environmental Systems, AIAA Technical Paper Number 2010-6187
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献