Suchoi / Sukhoi Su-24
Fighter Bomber
The Sukhoi Su-24 is a twin-engined two-seat sweep wing jet fighter bomber aircraft developed by the Soviet Design Bureau Sukhoi.
Propulsion | 2 Turbofan Engines |
Engine Model | Lyulka AL-21F-3A |
Engine Power (each) dry/with Afterburner | 75,0 / 109,8 kN | 16860 / 24684 lbf |
Speed | 2321 km/h | 1253 kts 1442 mph |
Service Ceiling | 17.500 m | 57.415 ft |
Range | 2.500 km | 1.350 NM 1.554 mi. |
Empty Weight | 19.000 kg | 41.888 lbs |
max. Takeoff Weight | 39.700 kg | 87.523 lbs |
Wing Span | 17,63 m | 57 ft 10 in |
Wing Area | 42,0 m² | 452 ft² |
Length | 24,53 m | 80 ft 6 in |
Height | 6,19 m | 20 ft 4 in |
First Flight | 05/1970 |
Production Status | out of production |
Total Production | ca. 1400 |
ICAO Code | SU24 |
NATO Code | Fencer |
Data for (Version) | Sukhoi / Suchoi Su-24M |