FIELD: aviation and astronautics.
SUBSTANCE: invention relates to the field of aviation and astronautics and relates to passenger aerospace aircraft. Aerospace aircraft comprises a fuselage, wings with ailerons, front empennage, cockpit, keel, air intake pipes, front elongated rectangular fairing, front wings on the front fairing, two pitot tubes, speed sensors. On the rear side of the fuselage, a combined power plant is installed, consisting of four turbojet three-circuit engines, inside the bodies of which there is a thermal chamber that ensures the operation of the engine at high altitudes, as well as RD-120 rocket engines for entering outer space, located inside the fuselage. In the front fairing there are braking solid propellant rocket engines (TRDs), upper vertical turbojets, left and right side turn turbojets and turbojets located below the fairing. In addition, the aircraft has rescue modules, the windows of which are located outside the fuselage.
EFFECT: reduced flight time.
1 cl, 25 dwg
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