TYPE: Advanced jet trainer/light attack jet
PROGRAMME: Revealed as feasibility study at Aviation Expo 2001, Beijing, September 2001.
DESIGN FEATURES: Shoulder-mounted wings with curved, leading-edge wingroot strakes; tandem cockpits; twin engines; single vertical fin well forward of slab tailplane.
FLYING CONTROLS: Assumed fly-by-wire.
POWER PLANT: Twin turbofans; possibly NMKB Progress AI-25s or domestic WS11s.
ACCOMMODATION: Two zero/zero ejection seats in tandem.
AVIONICS: HOTAS controls, HUD(s) and MFDs; stores management system.
|Wing span||11 m (36 ft)|
|Length overall||15 m (49 ft)|
|WEIGHTS AND LOADINGS:|
|Normal T-O weight, clean||6,500 kg (14,330 lb)|
|Max T-O weight||9,500 kg (20,950 lb)|
|Max level speed||M1.4|
|Max rate of climb at S/L||9,000 m (29,530 ft)/min|
|Service ceiling||16,000 m (52,490 ft)|