The upgraded single-seat armoured subsonic attack aircraft Su-25 is designed for close support of ground forces over the battlefield in daytime and at night, the targets being within visible range, as well as for support of installations with given coordinates on a 24-hour basis in all weathers.
| Aircraft performance | |
| Takeoff weight: | |
| - normal (with 2xFAB-500 + 2xR-73E), kg | 14,440 |
| - maximum, kg | 19,300 |
| Landing weight: | |
| - normal (without external ordnance and stores), kg | 11,020 |
| - maximum, kg | 13,200 |
| Maximum ordnance load, kg | 4,000 |
| Service ceiling (without external ordnance and stores), km | 7 |
| Maximum flight speed at sea level (without external ordnance and stores), km/h | 950 |
| Max Mach (without external ordnance and stores) | 0.82 |
| G-limit (operational) | +6.5/-2.0 |
| Practical flight range without external ordnance and stores, km: | |
| - at sea level, km | 500 |
| - at height, km | 1,000 |
| - with 4 x PTB-800 (to be dropped), km | 1,850 |
| Take-off run: | |
| - with normal takeoff weight, m | 500 |
| - with maximum takeoff weight, m | 1,050 |
| Landing run: | |
| - with normal landing weight, m | 550 |
| - with maximum landing weight, m | 750 |
| Aircraft dimensions: | |
| - length, m | 15.05 |
| - wingspan, m | 14.5 |
| - height, m | 2 |
| Crew | 1 |
| Powerplant | |
| Number and type of engines | 2 x R-195 |
| Thrust in full power, kgf | 4,500 |
| Avionics | |
| 1. Attack and navigation system | |
| 1.1 Visualisation-of-information and control system composed of: | |
| 1.1.1. On-board digital device | |
| 1.1.2. Collimating aviation indicator | |
| 1.1.3. Multi-purpose colour LCD indicator | |
| 1.1.4. Output information generation block | |
| 1.1.5. Information input system block | |
| 1.1.6. Voltage control | |
| 1.1.7 Mapping information generation block | |
| 1.2. GPS system | |
| 1.3. Attitude and heading reference system | |
| 1.4. Short-range radiotechnical navigation system | |
| 1.5. Doppler navigator | |
| 1.6. Radio altimeter | |
| 1.7. Air data system | |
| 1.8. Laser target illuminator and rangefinder | |
| 1.9. Control signal generation equipment | |
| 2. Radio equipment: | |
| 2.1. Radio communications transceiver | |
| 2.2. Ground troops communications link set | |
| 2.3. Voice information equipment | |
| 2.4. IFF transponder | |
| 2.5. Automatic direction finder | |
| 2.6. Marker radio receiver | |
| 2.7. Aircraft responder | |
| 3. Electronic countermeasure equipment | |
| 3.1. Radar illumination warning station | |
| 3.2. Automatic device for passive jamming emission | |
| 3.3. Small-size active jamming transmitter (in pod) | |
| 4. Registration, monitoring and alarm instrumentation | |
| 4.1. Onboard system of video surveillance and information recording | |
| 4.1.1. Video recording system | |
| 4.1.2. Onboard system for recording of tactical employment results | |
| 4.2. Emergency warning system | |
| 4.3. On-board device for flight configuration recording | |
| 4.3.1. Onboard solid-state FLASH memory storage unit | |
| 4.4. Multi-function flight recorder | |
| 5. Weapons control system | |
| Armaments | |
| 1. Guns | Onboard 30mm gun with 250 rds |
| 2. Guided air-to-surface missiles | Kh-29L, Kh-25LD, (L) |
| 3. Guided air-to-air missiles | R-73E |
| 4. Incendiary bombs | ZB-500 |
| 5. Unguided missiles | Type: S-8, S-13, S-24, S-25 |
| 6. Air bombs: | 100, 250, 500 |
| 7. Small-size cargo pods | KMGU-2 |
| 8. External fuel tanks |
PTB-800 (840 l), PTB-1,150 (1,160 l) |
| 9. Suspension points | 11 |
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