FIELD: aircraft industry. SUBSTANCE: high- temperature coating contains, wt.%: silicon, 6-9; boron, 2-5; haffnium oxide, 63- 68; haffnium boride, 8-12; tantalum pentoxide, 12-17. Invention can be applied for oxidation protection of silicon carbide matrix-based nonmetallic materials with carbon fiber filler. EFFECT: increased antioxidant activity of carbon ceramic composites at temperature 1800 C. 2 tbl
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Authors
Dates
2002-09-20—Published
2000-12-07—Filed