Su-22M4

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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