In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB Petlyakov |
| COUNTRY | Russia |
| TYPE |
High-altitude fighter
|
| CREW | 3 |
| POWER-PLANT | Two piston engines Μ-105 with supercharger ΤΚ-2 |
| Power, h.p. | 2x1.100 |
| DIMENSIONS | |
| Length, m | 12,69 |
| Height, m | 3,95 |
| Wing span, m | 17,15 |
| Wing area, m2 | 40,50 |
| WEIGHT | |
| Maximum take-off, kg | 7.260 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 5.172 |
| Internal fuel, kg | - |
| Warload, kg | 1.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 535 |
| Max speed in low height, km/h | - |
| Cruising speed, km/h | 455 |
| Range, km | 1.400 |
| Combat range, km | - |
| Service ceiling, m | 12.200 |
| Rate of climb, m/min | 588 |
| Maximum overload, g | - |
| ARMAMENT | 2x20 mm cannons ShVAK, two 7,2 mm machine-gun ShKAS or up to 1.000 kg bombs. |