Supersonic aircraft for executing military mission, has delta wing provided with ailerons and flaps at ends of wing, aerodynamic pressure channel sealingly mounted at compressor, and air intakes provided with rack and pinion drive

摘要

The aircraft has a turbojet engine assembled with a posterior part of fuselage (1), and provided with a vertical tail group (2) and a delta wing (3). The wing is provided with ailerons (4) and flaps (5) at ends of the wing. A circular aerodynamic pressure channel (7) is transversely placed, and is sealingly mounted at a compressor (6) using a clamp type system. Air intakes (10) are provided with a rack and pinion drive (11). Two devices of large resistance are provided between the fuselage and channel, where the devices communicate with each other and with an outer part of the fuselage.