材料科学
分子动力学
无定形固体
原子氧
无定形二氧化硅
析氧
化学物理
氧气
化学工程
纳米技术
物理化学
计算化学
结晶学
有机化学
化学
电极
工程类
电化学
作者
Qiang Zhou,Hao Ren,Hongfei Ye,Haiying Han,Yonggang Zheng
标识
DOI:10.1021/acsami.4c16503
摘要
Using reactive molecular dynamics simulations, the protective limit, erosion mechanism, and surface mechanical properties of amorphous silica material under an extreme atomic oxygen (AO) impact are studied in this paper. The results show that the AO erosion process consists of two distinct stages: the absorption stage and the sublimation stages, with the transition occurring at a surface temperature of about 4200 K. High-energy and high-flux AO impacts shorten the duration of the absorption stage due to increased penetration (30 eV AO penetrating up to 4 Å of material), a high heating rate (230 K/ps), and enhanced chemical reactivity, leading to a reduction in material’s protective performance. Notably, amorphous silica demonstrates a superior protective capability against a high-energy (10 eV) AO impact with an oxygen particle erosion rate of only 27% after 100 ps. Nanoindentation simulations indicate that amorphous silica exhibits excellent vertical and lateral surface mechanical properties when the oxygen atoms on its surface reach a dynamic equilibrium state (approaching the absorption peak: n = 200). These findings provide valuable insights for the evaluation and design of an amorphous silica-protected protective coating for aerospace applications in a low-Earth orbit.
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