▎ 摘　　要

NOVELTY - The method (300) involves providing a mixture of carbon nanotubes, graphene, and silicon carbon nitride (302). The mixture is heated (304) to bond the carbon nanotubes and the grapheme. The silicon carbon nitride is sintered (306) in the mixture. The mixture is heated to first temperature to initiate chemical bonding between the carbon nanotubes and the graphene. The mixture is pressurized during heating of the mixture at second temperature to cause the sintering of the silicon carbon nitride in the mixture at the temperature that is below 1,000 degrees Celsius. USE - Method for forming a ceramic matrix composite structure (claimed) for use as a composite skin of objects. Uses include but are not limited to aircrafts, drones, missiles, vehicles and satellites. ADVANTAGE - The method enables supporting dispersion in reaching a homogenized state to avoid particle agglomeration, so that casting/pressing operations can form a uniform green body ready to be sintered for production of a sheet of ceramic matrix composite material. The method enables reinforcing a ceramic with multi-wall carbon nanotubes in a manner to reduce abrasion and heat resistance, thus improving strength, flexibility and protection against medium to high frequencies. DESCRIPTION OF DRAWING(S) - The drawing shows a flow diagram illustrating a method for forming a ceramic matrix composite structure. Method for forming ceramic matrix composite structure (300) Step for providing mixture of carbon nanotubes, graphene, and silicon carbon nitride (302) Step for heating mixture to bond carbon nanotubes and graphene (304) Step for sintering carbon nitride in mixture (306)