Palladium-coated kapton for use on dust detectors in low earth orbit: Performance under hypervelocity impact and atomic oxygen exposure

A. Dignam, P. Wozniakiewicz, M. Burchell, L. Alesbrook, A. Tighe, Agnieszka Suliga, J. Wessing, A. Kearsley, J. Bridges, J. Holt, Stuart Howie, Libby Peatman, Dennis Fitzpatrick
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引用次数: 1

Abstract

Observation of dust and debris in the near Earth environment is a field of great commercial and scientific interest, vital to maximising the operational and commercial life-cycle of satellites and reducing risk to increasing numbers of astronauts in Low Earth Orbit (LEO). To this end, monitoring and assessment of the flux of particles is of paramount importance to the space industry and wider socio-economic interests that depend upon data products/services from orbital infrastructure. We have designed a passive space dust detector to investigate the dust environment in LEO—the Orbital Dust Impact Experiment (ODIE). ODIE is designed for deployment in LEO for ∼1 year, whereupon it would be returned to Earth for analysis of impact features generated by dust particles. The design emphasises the ability to distinguish between the orbital debris (OD) relating to human space activity and the naturally occurring micrometeoroid (MM) population at millimetre to submillimetre scales. ODIE is comprised of multiple Kapton foils, which have shown great potential to effectively preserve details of the impacting particles’ size and chemistry, with residue chemistry being used to interpret an origin (OD vs. MM). LEO is a harsh environment—the highly erosive effects of atomic oxygen damage Kapton foil—requiring the use of a protective coating. Common coatings available for Kapton (e.g., Al, SiO2, etc.) are problematic for subsequent analysis and interpretation of OD vs. MM origin, being a common elemental component of MM or OD, or having X-ray emission peaks overlapping with those of elements used to distinguish MM from OD. We thus propose palladium coatings as an alternative for this application. Here we report on the performance of palladium as a protective coating for a Kapton-based passive dust detector when exposed to atomic oxygen and impact. When subjected to impact, we observe that thicker coatings suffer delamination such that a coating of <50 nm is recommended. Analysis of atomic oxygen exposed samples shows a thin 10 nm coating of palladium significantly reduces the mass loss of Kapton, while coatings of 25 nm and over perform as well as or better than other commonly used coatings.
用于近地轨道尘埃探测器的镀钯卡普顿:在超高速撞击和原子氧暴露下的性能
对近地环境中的尘埃和碎片的观测是一个具有重大商业和科学意义的领域,对于最大限度地延长卫星的业务和商业生命周期以及减少近地轨道上越来越多的宇航员所面临的风险至关重要。为此目的,监测和评估粒子通量对空间工业和依赖轨道基础设施数据产品/服务的更广泛的社会经济利益至关重要。设计了一种被动空间尘埃探测器——轨道尘埃撞击实验(ODIE),用于研究低轨道尘埃环境。ODIE的设计目标是在近地轨道上运行1年,然后返回地球,分析尘埃颗粒产生的撞击特征。该设计强调了区分与人类空间活动有关的轨道碎片(OD)和自然发生的微流星体(MM)在毫米至亚毫米尺度上的能力。ODIE由多个卡普顿箔组成,它已经显示出巨大的潜力,可以有效地保留影响颗粒的尺寸和化学成分的细节,残留化学成分被用来解释起源(OD与MM)。LEO是一个恶劣的环境-原子氧的高度侵蚀作用破坏卡普顿箔-需要使用保护涂层。可用于Kapton的常见涂层(例如Al, SiO2等)对于随后的OD与MM来源的分析和解释是有问题的,作为MM或OD的共同元素成分,或者与用于区分MM和OD的元素的x射线发射峰重叠。因此,我们提出钯涂层作为这种应用的替代方案。在这里,我们报告了当暴露于原子氧和冲击时,钯作为卡普顿基被动粉尘探测器的保护涂层的性能。当受到冲击时,我们观察到较厚的涂层会发生分层,因此建议使用<50 nm的涂层。原子氧暴露样品的分析表明,10纳米薄的钯涂层显著降低了卡普顿的质量损失,而25纳米及以上的涂层的性能与其他常用涂层一样好或更好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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