FIELD: rocket and space equipment.
SUBSTANCE: subject of invention is heat-shielding coating of housing of high-speed aircraft, made of multilayer carcass, wherein frame is made in form of inner layer, which is a one-piece volume-reinforced preform of specified thickness of carbon, or silica, or quartz threads and two and more outer layers of specified thickness, made of heat-resistant fabric of carbon or silica or quartz threads, wherein inner and outer layers of frame are pierced by carbon, or silica, or quartz fibers.
EFFECT: proposed heat-shielding coating of high-speed aircraft body.
1 cl, 1 dwg
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