| Type |
Single seat fighter |
| Engine |
1 Shvetsov M-82FN with 3-bladed constant-speed propeller |
| Dimensions |
Length 8,67 m , height 2,54 m, span 9,8 m , wing area 17,5 m2 . Airfoil: root: NACA 23016; tip: NACA 23010 |
| Weights |
Empty 2706 kg, loaded 3168 kg , max. take off weight 3402 kg, fuel 345 kg , oil 50 kg |
| Performance |
Max.. speed 648 km/h at 6250 m , 583 km/h at sea level, landing speed 138 km/hcruising speed , range 765 km, endurance , service ceiling 11000 m , climb 16,7 m/sec., to 5000 m5 min. 12 sec. |
| Armament |
2 20 mm ShVAK cannon with 170 rpg . Bombs: 2 bombs up to 100 kg each |
