FIELD: protective coat production for inorganic fibrous constructive composites used in spacecraft and machine engineering industry.
SUBSTANCE: claimed coat contains (wt %): SiO2 - 0.1-10; SiB4 - 0.1-0.5; MoSi2 - 0.2-5; SiC - 1/5-10; and balance: Si3C5H15O0.25. Protective coat of present invention make it possible to obtain composites with operating temperature up to 1600°C.
EFFECT: protective coat with increased flowability on composite, thermal resistance and improved durability.
2 tbl
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Authors
Dates
2005-04-10—Published
2003-08-26—Filed