Su-24

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Origin:	Soviet Union
Prototype:	maiden flight July 2,1967
History:	variable-sweep wing NATO reporting name: Fencer in service since 1974, tests with many casualties
Crew:	2
Powerplant:	2 x Saturn/Ljulka AL-21F-3A turbojet engines with thrust á 75 kN, afterburning á 109 kN
Performance:	max speed Mach 1.35 combat radius 615 km ferry range 2,775 km service ceiling 11,000 m fuel capacity 11.1 t rate of climb 150 m/s thrust/weight: 0.60 G-force limit 6G takeoff roll 1,550 m, landing roll 1,100 m
Weight:	empty weight 22.3 t, max takeoff weight 43.75 t
Dimensions:	length 22.53 m, wingspan10.37-17.64 m, height 6.19 m, wing area 55.2 m2
Armament:	jet equipment, rockets, bombs, self-defence air-to-air missiles, etc.
Versions:	numerous versions, number built 1,400
Operators:	Russia + 10 other states

https://en.wikipedia.org/wiki/Sukhoi_Su-24