Su-25KM Scorpion [Georgia]
| Crew | 1 man |
| Length | 15,53 m |
| Roll | 14,36 m |
| Height | 4,80 m |
| Net wing area | m2 30,10 |
| Weight of an empty aircraft | kg 9100 |
| Takeoff weight | Normal, kg 14520 - Maximum, kg 17500 |
| Landing weight: |
- Normal, kg 11000 - Maximum, kg 12100 |
| Maximum military load | kg 4500 |
| Supply of the fuel produced in internal tanks | 3660 liters |
| Capacity of additional fuel tanks | ???-800 (4 pcs.), l 820 each |
| Capacity of additional fuel tanks | ???-1150 (2 pcs.), l 1160 each |
| Type and number of engines | 2 ??? ?-195 |
| Emergency traction force | , kg.force 2 ? 4500 |
| Practical ceiling | m 7000 |
| Maximum speed |
- At the ground, km/h 950 - At height, km/h ?=0.82 |
| Practical range ability |
- At the ground, km/h 495 - At height, km/h 1000 - From 4????-800, km 1980 |
| Takeoff roll |
- With normal takeoff mass, m 500 - With maximum takeoff mass, m 1050 |
| Landing roll |
- With normal landing mass, m 550 - With maximum landing mass, m 750 |
| Maximum working load +6,5/-2,0 | |
| Armament | |
| Gun armament |
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| Missiles armament |
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| Bomber armament |
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| Number of suspension centers | 10 |
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