FIELD: aeronautical engineering.
SUBSTANCE: invention relates to aviation, namely to passenger supersonic sweep forward aircrafts with rescue modules. The aircraft comprises fuselage, landing gear, two wings with ailerons, power plant including four lift-thrust turbojet engines attached to the wing with its nozzle backward. Each wing is attached to fuselage to turn horizontally relative to the fuselage axis through 53°. The aircraft comprises also the nose horizontal tail unit that can horizontally turn parallel to the fuselage axis, as well as horizontal and vertical tail units. The fuselage comprises the passenger emergency-and-rescue ejection modules and cockpit with ejection seta.
EFFECT: higher reliability and safety in flight and in emergency, lower fuel consumption during take-off and landing.
5 cl, 13 dwg
