Zhao Wang, Wei Qiang, Huang Chuanjin, Zhu Yaoshun, Hu Ning
Key Laboratory of Hebei Province on Scale-Span Intelligent Equipment Technology, School of Mechanical Engineering, Hebei University of Technology, Tianjin 300401, China.
State Key Laboratory of Reliability and Intelligence Electrical Equipment, Hebei University of Technology, Tianjin 300401, China.
Polymers (Basel). 2022 Dec 12;14(24):5444. doi: 10.3390/polym14245444.
Kapton film is a polymeric material widely used on low-Earth-orbit (LEO) spacecraft surfaces. In the LEO environment, atomic oxygen (AO) is spaceflight materials' most destructive environmental factor. The erosion mechanism of AO on Kapton films has long been an important issue, where the parameter dependence of the AO effect has received increasing attention. Studies of AO energy and cumulative flux have been extensively carried out, while the influence mechanism of the incidence angle and flux density is not fully understood. The AO incidence angle and flux density in space are diverse, which may cause different damage effects on aerospace materials. In this paper, the dependence of the incidence angle and flux density in the damaging effect of AO on Kapton films was investigated using ground-based AO test technology and the reactive molecular dynamics (ReaxFF MD) simulation technique. Firstly, the ground-based experiment obtained the mass loss data of Kapton films under the action of AO with a variable incidence angle and flux density. Then, the mass loss, temperature rise, product, and erosion yield of Kapton during AO impact with different incidence angles and dose rates were calculated using the ReaxFF MD method. The influences of the incidence angle and flux density on the damage mechanism of the AO effect were discussed by comparing the simulation and test results. The results show that the AO effect in the lower incidence angle range (0-60°) is independent of the incidence angle and depends only on the amount of impacted atomic oxygen. AO in the higher incidence angle range (60-90°) has a surface stripping effect, which causes more significant mass loss and a temperature rise while stripping raised macromolecules from rough surfaces, and the erosion effect increases with the increasing incidence angle and amount of impacted atomic oxygen. There is a critical value for the influence of flux density on the AO effect. Above this critical value, AO has a reduced erosive capacity due to a lower chance of participating in the reaction. The amount of each main product from the AO effect varies with the incidence angle and flux density. Nonetheless, the total content of the main products is essentially constant, around 70%. This work will contribute to our understanding of the incidence angle and flux density dependence of the AO effect and provide valuable information for the development of standards for ground simulation tests.
聚酰亚胺薄膜是一种广泛应用于近地轨道(LEO)航天器表面的聚合材料。在近地轨道环境中,原子氧(AO)是对航天材料最具破坏性的环境因素。长期以来,原子氧对聚酰亚胺薄膜的侵蚀机制一直是一个重要问题,其中原子氧效应的参数依赖性受到了越来越多的关注。关于原子氧能量和累积通量的研究已经广泛开展,而入射角和通量密度的影响机制尚未完全明确。太空中的原子氧入射角和通量密度各不相同,这可能会对航天材料造成不同的损伤效应。本文利用地面原子氧测试技术和反应分子动力学(ReaxFF MD)模拟技术,研究了原子氧对聚酰亚胺薄膜损伤效应中入射角和通量密度的依赖性。首先,地面实验获得了在可变入射角和通量密度的原子氧作用下聚酰亚胺薄膜的质量损失数据。然后,使用ReaxFF MD方法计算了不同入射角和剂量率下原子氧冲击聚酰亚胺过程中的质量损失、温度升高、产物和侵蚀产率。通过比较模拟和测试结果,讨论了入射角和通量密度对原子氧效应损伤机制的影响。结果表明,在较低入射角范围(0 - 60°)内,原子氧效应与入射角无关,仅取决于撞击的原子氧量。在较高入射角范围(60 - 90°)内,原子氧具有表面剥离效应,会导致更显著的质量损失和温度升高,同时从粗糙表面剥离凸起的大分子,侵蚀效应随入射角和撞击原子氧量的增加而增强。通量密度对原子氧效应的影响存在一个临界值。高于此临界值,原子氧参与反应的机会降低,侵蚀能力减弱。原子氧效应各主要产物的量随入射角和通量密度变化。尽管如此,主要产物的总含量基本恒定,约为70%。这项工作将有助于我们理解原子氧效应的入射角和通量密度依赖性,并为地面模拟试验标准的制定提供有价值的信息。