Hypersonic-speed heat-proof bearing integrated light empennage

The hypersonic-speed heat-proof bearing integrated light empennage comprises an empennage body, an empennage front edge and an empennage rear edge, the empennage body is longitudinally fixed to the tail of an aircraft, and the end face of the lower end of the empennage body is fixedly connected with the aircraft; the wing front edge is obliquely arranged and fixedly connected with the front end of the wing body, the wing rear edge is obliquely arranged and fixedly connected with the rear end of the wing body, and the wing body comprises an internal framework and an external skin wrapping the internal framework; according to the invention, the wing body is designed into a structure comprising the internal framework and the external skin, and the internal framework is hollowed out, so that the weight of the empennage can be effectively reduced, the empennage is lightened to the greatest extent, and the carrying pressure is reduced; the empennage front edge and the empennage rear edge which are independent are i