Basic specifications
thrust-vectoring engines producing thrust in special power conditions, kgf
2x14,500
max weapon load, kg
8,000
service ceiling, km
18
max airspeed (horizontal flight) H = 200 m, km/h
1,400
max airspeed (horizontal flight) H = 11,000 m, max number, M
2.25
takeoff run with normal takeoff weight (at full afterburner), m
400-450
landing run with drag chute, m
650-700
max maneuver load, g
9
crew
1