Optical and electrophysical properties of nitride TiAlSiN and carbonitride TiAlSiCN coatings: influence of reactive magnetron deposition regimes

S. Konstantinov, F. F. Komarov, I. V. Chizhov, V. A. Zaikov
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Abstract

The development of thin-film thermal control coatings for small spacecraft is relevant. Coatings based on titanium nitride are capable of functioning in unfavorable conditions of near and deep space, due to their high resistance to the irradiation by high-energy particles. Using the reactive magnetron sputtering method, the nanostructured TiAlSiN and TiAlSiCN coatings were formed on the substrates of silicon oxide (SiO2), glass-ceramic CT-1 and single-crystalline silicon (Si(100)). A study of the electrophysical and optical properties of the formed coatings was carried out. The deposited coatings demonstrate a good reflectivity in the infrared range of spectrum (700–2000 nm), what is important for reducing the overheating of the spacecraft (SC) under the influence of the direct sunlight. In the visible range of spectrum (400–700 nm), a low level of total Rtotal reflection is observed. This is promising for satellites designed to observe the Earth’s surface. The values of solar absorption coefficients αs, emissivity coefficients ε0, ratios αs/ε0, as well as the equilibrium temperature Tр for the samples under study were obtained. The values of resistivity ρ and surface resistance R□, electron concentration N and electron mobility μ were determined. It has been discovered that TiAlSiN, TiAlSiCN films are electrically conductive: ρTiAlSiN = (92÷4260) ∙ 10–7 Ω ∙ m, ρTiAlSiCN = (51÷2360) ∙ 10–7 Ω ∙ m. It has been found that adding carbon to the coating composition reduces the resistance. The obtained nanostructured coatings of TiAlSiN nitride and TiAlSiCN carbonitride can be used as temperature control coatings for small spacecrafts.
氮化 TiAlSiN 和碳氮化 TiAlSiCN 涂层的光学和电物理特性:反应磁控沉积制度的影响
为小型航天器开发薄膜热控涂层具有现实意义。基于氮化钛的涂层能够在近太空和深空的不利条件下发挥作用,因为它们具有很强的抗高能粒子辐照的能力。利用反应磁控溅射法,在氧化硅(SiO2)、玻璃陶瓷 CT-1 和单晶硅(Si(100))基底上形成了纳米结构的 TiAlSiN 和 TiAlSiCN 涂层。对所形成涂层的电物理和光学特性进行了研究。沉积的涂层在红外光谱范围(700-2000 纳米)内具有良好的反射性,这对于减少航天器(SC)在阳光直射下的过热现象非常重要。在可见光谱范围(400-700 纳米)内,观察到的总反射率较低。这对于设计用于观测地球表面的卫星来说很有希望。研究中的样品的太阳吸收系数 αs、发射率系数 ε0、比率 αs/ε0 以及平衡温度 Tр 的值均已获得。测定了电阻率 ρ 和表面电阻 R□、电子浓度 N 和电子迁移率 μ 的值。研究发现 TiAlSiN 和 TiAlSiCN 薄膜具有导电性:ρTiAlSiN = (92÷4260) ∙ 10-7 Ω ∙ m,ρTiAlSiCN = (51÷2360) ∙ 10-7 Ω ∙ m。获得的氮化 TiAlSiN 和碳氮化 TiAlSiCN 纳米结构涂层可用作小型航天器的温度控制涂层。
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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