SU-24MR
Font-line reconnaissance plane

	Specification:
	Year deployed Wing span, m - maximum - minimum Length, m Height, m Wings area, m2 - maximum - minimum Weight, kg - empty aircraft - normal take-off - maximum take-off Fuel, kg - internal - AFT Engine Thrust, kN - dry - afterburner Maximum speed, km/h - in altitude - on sea level Range, km Combat radius, km Service ceiling, m Crew Armament:	- 1983 - 17,63 - 10,36 - 24,53 - 6,19 - 55,17 - 51,02 - 19200 - 39700 - 28000 - 16440 - 11700 - 39700 (4 У 1250  or 2 У 3000 l) - 1 TJEA AL-21-F-гA - 76.49 - 110.32 - 2240  - 1400  - 3800 - 410-1300 - 17500  - 1 Warload - 8000 kg in 8 hardpoints 2 AAM R-60, reconnaissance and ECM pods