Su-22M4

Origin: Soviet Union
Prototype: maiden flight August 2,1966
History:
  • variable-sweep wing
  • Su-17/ -20/ -22 family
  • produced 1969-1990, in armament since 1970
  • successful export article
  • participated in a number of military conflicts
Crew: 1
Powerplant: 1 x Ljulka AL-21F-3 turbojet engine with thrust 76.4 kN and afterburning 109.8 kN
Performance:
  • max speed Mach 2, sea level 1,400 km/h
  • combat radius 1,150 km
  • ferry range 2,300 km
  • service ceiling 14,200 m
  • rate of climb 230 m/s
  • fuel capacity 3,770 kg
  • thrust/weight 0.68
  • G-force limit 7G
Weight: empty weight 12.16 t, max takeoff weight 28 t
Dimensions: length 19.02 m, wingspan 10.02-13.68 m, height 5.12 m, wing area 34.5-38.5 m2
Armament: 2×30 mm cannons, jet equipment, rockets, bombs, in total 4 t
Versions: numerous versions; number built 2,867
Operators: 23 states

https://en.wikipedia.org/wiki/Sukhoi_Su-17