FIELD: aviation.
SUBSTANCE: group of inventions relates to aircraft intended for delivery of missile weapons. Piloted or unmanned cruise missile carrier (MC) in the first version includes central fuselage module, power plant of jet cruise engines and run-and-acceleration-landing engines, an integrated control system, two pairs of wings with mechanization elements arranged at different levels in the nose and tail parts of the fuselage central module, consisting of the main wing profile and additional extensible wing elements. MC includes active and passive thermal protection systems. Reactive mid-flight engines are made straight-flow air-jet and are located in tail part of fuselage central module. Run-and-acceleration-landing engines are made turbojet and are installed in fore part along sides of fuselage. MC in the second version includes mid-flight LPE engines.
EFFECT: group of inventions is aimed at creation of optimal layout MC, capable of high-speed, high maneuverability of cruise missiles.
2 cl, 28 dwg
