Heat-resistant slip coatings of the ZrB₂–MoSi₂–SiC system on CCCM were examined for protection of aerospace technology elements from oxidation. The following compositions (mass%) were studied as coating materials: 55 ZrB₂ + 25 MoSi₂ + 20 SiC (ZSM25), 50 ZrB₂ + 30 MoSi₂ + 20 SiC (ZSM30), and 45 ZrB₂ + 35 MoSi₂ + 20 SiC (ZSM35). Heat-treatment modes were elaborated for the coatings. The optimal method for producing heat-resistant coatings was selected. The ZSM25 coating was found to satisfy the heat-resistance assessment tests conditions in a Multiplaz 2500-m plasmatron for 20 sec at an angle of 45°, presumably by forming a highly viscous ZrSiO₄ film.

检查了CCCM上ZrB ₂ -MoSi ₂ -SiC系统的耐热滑爽涂料，以保护航空航天技术元素免受氧化。研究了以下组成（质量％）作为涂层材料：55 ZrB ₂ + 25 MoSi ₂ + 20 SiC（ZSM25），50 ZrB ₂ + 30 MoSi ₂ + 20 SiC（ZSM30）和45 ZrB ₂ + 35 MoSi ₂+ 20 SiC（ZSM35）。阐述了涂层的热处理方式。选择了生产耐热涂层的最佳方法。发现ZSM25涂层在Multiplaz 2500-m等离子加速器中以45°角满足20秒的耐热性评估测试条件，大概是通过形成高粘性的ZrSiO ₄膜来实现的。