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 |