期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
A reaction-diffusion model for atomic oxygen interacting with spacecraft surface protective materials in low earth orbit environment 被引量:2
1
作者 LEE Chun-Hian 《Science China(Technological Sciences)》 SCIE EI CAS 2009年第4期1125-1134,共10页
When hyperthermal atomic oxygen collides with a silicon surface, an ultrathin oxidation regime characterized by fractional atomic-oxygen anions having low diffusive and reactive barriers, along with their enhanced dif... When hyperthermal atomic oxygen collides with a silicon surface, an ultrathin oxidation regime characterized by fractional atomic-oxygen anions having low diffusive and reactive barriers, along with their enhanced diffusion due to both the electric field and image potential, will form on the surface. In ac- cordance with these properties, an attempt was made in the present study to modify the Almeida- Goncalves-Baumvol (AGB) model by setting the diffusivity and reaction rate constant to be diffu- sion-length dependence. According to the modified model, numerical parametric studies for oxidation thin growth were performed. The dependencies of the diffusion coefficient, the reaction rate constant, the attenuation length, and the adjustable parameter upon the translational kinetic energy, flux, tem- perature, and tangential flux of atomic oxygen were analyzed briefly via the fitting of the experimental data given by Tagawa et al. The numerical results confirmed the rationality of the modified diffu- sion-reaction model. The model together with the computer code developed in this study would be a useful tool for thickness evaluation of the protective film against the oxidation of atomic oxygen toward spacecraft surface materials in LEO environment. 展开更多
关键词 hyperthermal atomic oxygen silicon REACTION-DIFFUSION EQUATIONS OXIDATION thickness numerical simulation
原文传递
原子氧对碳纤维增强氰酸酯复合材料的侵蚀及机理研究 被引量:2
2
作者 杨阳 徐辉 +3 位作者 石佩洛 武博涵 王黑龙 车丽 《宇航材料工艺》 CSCD 北大核心 2017年第5期56-60,共5页
针对碳纤维增强氰酸酯复合材料(CFCE)开展原子氧暴露试验及反应产物原位测量的散射试验,并进行暴露前后的质量损失、SEM及XPS试验。结果表明,该材料的受原子氧腐蚀率为(2.20±0.36)×10^(-24)cm^3/atoms。受原子氧腐蚀后,样品表... 针对碳纤维增强氰酸酯复合材料(CFCE)开展原子氧暴露试验及反应产物原位测量的散射试验,并进行暴露前后的质量损失、SEM及XPS试验。结果表明,该材料的受原子氧腐蚀率为(2.20±0.36)×10^(-24)cm^3/atoms。受原子氧腐蚀后,样品表面C元素相对原子浓度增加,O元素基本不变;表面的树脂脱落,碳纤维暴露在原子氧环境中,表面出现蚀坑,且数量及形状逐渐变大,蚀坑相连,最终沿纤维方向形成一条沟壑。高能氧原子与复合材料发生反应,生成产物CO、CO_2、H_2O、OH和CH_3。 展开更多
关键词 碳纤维增强氰酸酯复合材料 原子氧暴露试验 散射试验 SEM试验 XPS试验
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部