The upgraded front-line bomber Su-24MK is designed for bombardment with bombs and missiles in favourable and adverse weather conditions, in daytime and at night, including at low altitudes with pinpoint destruction of ground and naval surface targets.
| Aircraft performance | |
| Takeoff weight: | |
| - normal, kg | 38,040 |
| - maximum, kg | 43,755 |
| Maximum landing weight, kg | 27,900 |
| Maximum internal fuel, kg | 11,100 |
| Normal ordnance load, kg | 3,000 |
| Maximum ordnance load, kg | 8,000 |
| Service ceiling (without external ordnance and stores), km | 11 |
| Maximum flight speed at sea level (without external ordnance and stores), km/h | 1,315 |
| Max Mach (without external ordnance and stores) | 1.35 |
| G-limit (operational) | 6 |
| Operational radius of action at sea level in mixed mode (Vcr in the 200-km area, V=900 km/h in other areas) with PTB external fuel tanks and 6x FAB -500M-62 bombs, km | 615 |
| Ferry flight range with 2xPTB-3000 external fuel tanks, km: | |
| - with PTB external fuel tanks dropped | 2,775 |
| - with one in-flight refuelling | 5,000 |
| Takeoff run at normal take-off weight, m | 1,550 |
| Landing run at normal landing weight (with braking parachute), m | 1,100 |
| Aeroplane dimensions: | |
| - length, m | 24.532 |
| - wingspan, m | 17.638 (10.366) |
| - height, m | 6.193 |
| Crew | 2 |
| In-flight refuelling system | |
| Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min | 1,100 |
| Powerplant | |
| Number and type of engines | 2 x AL-21FZA |
| Thrust: | |
| - in afterburner, kgf | 111,200 |
| - at full power, kgf | 11,200 |
| Avionics | |
| 1. Attack and navigation system | |
| 1.1. Digital computer device | |
| 1.2. Doppler navigator | |
| 1.3. Optical sighting device | |
| 1.4. I/O device (I/O) | |
| 1.5. On-board switchgear (OBS) | |
| 1.6. Photo recording equipment set | |
| 1.7. Control signal conditioner | |
| 1.8. Onboard module of Tekon-1 television guidance system | |
| 1.9. Laser/TV search and track system (LTVSTS) | |
| 1.10. Radio command linkage | |
| 1.11. Passive radar: | |
| - letter A and A' instrumentation pod | |
| - letter B, B' and C instrumentation pod | |
| 1.12. Nose radar scanner (NRS) | |
| 1.13. Collision-warning radar (CWR) | |
| 1.14. Small-size inertial instrument system | |
| 1.15. Low-range radio altimeter | |
| 1.16. NRS video signal onboard processing block | |
| 1.17. TV display | |
| 1.18. GPS satellite-based navigation system | |
| 2. Autopilot system | |
| 3. IFF equipment | |
| 4. VHF-UHF communications transceiver | |
| 5. Short-wave radio | |
| 6. Automatic direction finder | |
| 7. Aircraft responder | |
| 8. Electronic countermeasures system | |
| 8.1. Radar warning receiver | |
| 8.2. Jamming capabilities control device | |
| 8.3. Active jamming system | |
| 8.4. Infrared search and track sensor (IRSTS) | |
| 8.5. Cartridge ejection mechanism | |
| 9. Integrated defensive aids suite | |
| 10. Long-range radiotechnical navigation system | |
| 11. Short-range radiotechnical navigation system | |
| 12. Flight data recorder system | |
| 13. Camera | |
| 14. Tape-recording mechanism, solid-state storage unit | |
| 15. Combat performance monitoring equipment | |
| 16. VCR | |
| 17. Weapons control system | |
| Armaments | |
| 1. Guns | Onboard 23mm gun with 500 rds |
| 2. Guided air-to-surface missiles |
Kh-25ML Kh-25MR (Kh-23M) Kh-29L Kh-29T Kh-58E, Kh-58E-01 (lit. A, A', B, C) Kh-31P (lit. A, A', B, B', C) Kh-31A Kh-59, Kh-59ME S-25LD |
| 3. Guided air-to-air missiles | R-60MK (R-60), R-73E |
| 4. Guided bomb units | KAB-500KR, KAB-500L |
| 5. Air bombs: |
AB-100 AB-250 (M54) AB-250 (M62) AB-500M-54 ODAB-500PM |
| 6. Cluster bombs |
RBK-250 RBK-500 |
| 7. Incendiary bombs | S-24B |
| 8. Unguided missiles: | S-25-OFM |
| 9. Small-size cargo pods | KMGU-2 |
| 10. Pod guns | SPPU-6 |
| 11. External fuel tanks |
PTB-2,000 (1,860 l), PTB-3,000 (3,050 l) |
| 12. Suspension points | 8 |
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