In numbers Through the lens Video
Su-24MK frontline bomber export version (1987) which was exported to Algeria, Iraq, Libya and Syria.
Three-view drawing
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY | Russia |
| TYPE |
Front-line bomber
|
| CREW | 2 |
| POWER-PLANT | Two turbojet engines NPO Saturn Al-21-F-3A |
| Thrust, kgf | 2x11.250 |
| DIMENSIONS | |
| Length, m | 24,59 |
| Height, m | 6,19 |
| Wing span, m | - |
| - maximum (69ο) | 17,64 |
| - minimum (16ο) | 10,37 |
| Wing area, m2 | - |
| - minimum | - |
| - maximum | - |
| WEIGHT | |
| Maximum take-off, kg | 39.700 |
| Normal take-off, kg | 33.590 |
| Empty aircraft, kg | 22.320 |
| Internal fuel, kg | 9.800 |
| Weight of transported fuel with external tanks, l. | up to 6.610 |
| Warload, kg | 8.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude 11.000 m), km/h | 1.700 |
| Maximum speed, sea level km/h | 1.400 |
| Maximum speed in low height, km/h | - |
| Range, km | - |
| Combat range, km | |
| - without external fuel tanks | 390-570 |
| - with external fuel tanks | 1.250 |
| Service ceiling, m | 11.000 |
| Maximum overload, g | 6,5 |
| ARMAMENT | 1x30 mm six-barrel cannon GSh-6-23M with 500 rounds. Number external hardpoints: 8. Transportation of weapons: Air-to-surface missile Kh-23, Kh-23M, Kh-28, Kh-25MR, Kh-25ML, Kh-29L, Kh-29T, Kh-31P, Kh-58U, Kh-58E, Kh-59. Air-to-air two R-60 or R-60M. Guided Air Bomb KAB-500L, KAB-500KR, KAB-1500L. Free fall bombs FAB-100, FAB-250, FAB-500M62, FAB-500M54, 3B-500Sh, 3B-500GD, RBK-250, RBK-500. 3x pods SPPU-6 with six-barrel cannons GSh-6-23M or 9A-798 (23 mm, 3x400 rounds) or pods KMGU. Rokets S-5, S-8KO, S-13T, S-130F, S-24B, S-250F, S-250FM. |