FIELD: aviation.
SUBSTANCE: in the first version, a manned or unmanned accelerating carrier aircraft includes a central integrated body shape airframe, a chassis, a combined power plant from jet engines, an integrated control system with elements of a reactive control system, bearing consoles of wings with elements of mechanization, systems of active and passive thermal protection of external structural elements. Proposed power plant consists of bypass turbofan engine or afterburning turbojet engine to accelerate aircraft carrier and rocket engines with liquid fuel or solid fuel. Nozzles of mid-flight engines are located on end of tail part of fuselage of carrier aircraft. Orbital carrier rocket is arranged inside fuselage body. In the second version, carrier aircraft is equipped with accelerators with possibility of autonomous vertical or horizontal landing.
EFFECT: group of inventions is aimed at creation of reliable and energetically effective reusable aerospace system.
2 cl, 40 dwg
