In numbers Through the lens Video
The Su-24MR air reconnaissance frontline aircraft.
Three-view drawing
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY | Russia |
| TYPE |
Reconnaissance
|
| CREW | 2 |
| POWER-PLANT | Two turbojet engines NPO Saturn Al-21-F-3A |
| Thrust, kg | 2x11.250 |
| DIMENSIONS | |
| Length, m | 24,53 |
| 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 | 33.300 |
| Empty aircraft, kg | 22.100 |
| Internal fuel, kg | 9.800 |
| Weight of transported fuel with external tanks, l. | 4x1.250 or 4x3.000 |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 1.430 |
| Maximum speed, sea level km/h | - |
| Maximum speed in low height, km/h | 1.320 |
| Range, km | - |
| Combat range, km | 650 |
| Service ceiling, m | 11.000 |
| Maximum overload, g | - |
| ARMAMENT | Two air-to-air missile R-60, reconnaissance and ECM pods. |