Technical specifications 
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TECHNICAL SPECIFICATIONS
| DESIGNER | Myashichev |
| COUNTRY | Russia |
| TYPE | Heavy fighter |
| CREW | 2 |
| POWER-PLANT | Two reciprocating motor VK-107A |
| Power, h.p. | 2 x 1.550 |
| DIMENSIONS | |
| Length, m | 13,795 |
| Height, m | 3,95 |
| Wing span, m | 18,11 |
| Wing area, m2 | 43,80 |
| WEIGHT | |
| Normal take-off, kg | 9.850 |
| Empty aircraft, kg | 7.300 |
| Maximum take-off, kg | 11.700 |
| Internal fuel, kg | 1.675/3.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 627 |
| Cruising speed, km/h | - |
| Max speed in low height, km/h | 531 |
| Rate of climb, m/min | - |
| Service ceiling, m | 9.600 |
| Range, km | 1.700 |
| Combat range, km | - |
| ARMAMENT | Two 20 mm cannons B-20, two 37 mm cannons NS or two 45 mm cannons NS, two 20 mm cannons BT-20. |
