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Specifications - Yak-130 Combat Trainer, Russia
| Dimensions |
| Length, Development Model | 11.49m |
| Length, Production Model | 11.245m |
| Height | 4.76m |
| Wingspan | 9.72m |
| Wing Area | 23.52mē |
| Wing Aspect Ratio | 4:1 |
| Weights |
| Empty Weight | 4,600kg |
| Typical Training Configuration Weight | 5,700kg |
| Maximum Take-Off Weight | 9,000kg |
| Weapon Payload | 3,000kg |
| Internal Fuel | 1,750kg |
| Engines |
| Type (Prototype) | 2 x V-2S turbofan engines |
| Thrust (Prototype) | 2,200kg each |
| Type (Production Aircraft) | 2 x AI-222-25 turbofan engines |
| Thrust (Production Aircraft) | 2,500kg each |
| Performance |
| Maximum Level Speed | 1,060km/h |
| Service Ceiling | 12,500m |
| Range With Internal Fuel | 2,000km |
| Sustained G-limit at Mach 0.8 | +4.8G |
| g-Limit | +8g to -3g |
| Landing Speed | 190km/h |
| Landing Run | 670m |
| Take-Off Speed | 210km/h |
| Take-Off Run | 380m |
| Service Life | 30 years |
| Flight Hours | 10,000 extendable to 15,000 |
| Landings | 20,000 landings |