FIELD: aviation equipment.
SUBSTANCE: invention relates to the field of aviation technology, in particular, to structures of vertical take-off and landing aircraft. Supersonic low-profile plane of vertical take-off and landing (SLPVTOL) is equipped at the ends of the outer sides of the tail beams with side steering nozzles (SSN), acting in the horizontal plane alternately, changing the balance on the course when working two lifting fans (LF). Control system is made with two lift-marching TJE with power take-off for the drive of two LFs and thrust-vectoring module (TVM) to create lift and pitch control moments when performing VTOL and hovering, and thrust during horizontal flight in the configuration of a supersonic plane. SLPVTOL is made according to the integrated aerodynamic scheme of the longitudinal triplane with the horizontal canard (HC), delta midwing (DMW) and V-shaped tail, and with the ability to transform its flight configuration after performing the STOL or VTOL from the corresponding aircraft with two LFs, two TJEs with TVM and SSN in a trans-or supersonic plane.
EFFECT: reduced visibility, increased speed and range.
3 cl, 1 dwg, 1 tbl
