FIELD: chemistry.
SUBSTANCE: invention relates to a composite material based on carbon and a process of its production, which may be used in the rocket and space and aviation industries. Method involves stressing and heat treating of the fullerene C60 mixture, a sulfur-containing compound CS2 and filler, with the use of carbon nanotubes as the filler.
EFFECT: technical result consists in the production of a high-hard, heat-resistant and light composite material with a tensile strength at transverse bending of not less than σ*bend=700MPa for the manufacture of articles.
2 cl, 3 ex
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