Technical specifications 
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TECHNICAL SPECIFICATIONS
| DESIGNER | OKB Tupolev |
| COUNTRY | Russia |
| TYPE | Front-line Bomber |
| CREW | 3 |
| POWER-PLANT | Two reciprocating motor AM-37 |
| Power, h.p | 2 x 1.400 |
| DIMENSIONS | |
| Length, m | 13,72 |
| Height, m | 4,94 |
| Wing span, m | 18,80 |
| Wing area, m2 | 48,50 |
| WEIGHT | |
| Normal take-off, kg | 10.448 |
| Empty aircraft, kg | 7.823 |
| Maximum take-off, kg | 11.428 |
| Internal fuel, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 610 |
| Cruising speed, km/h | - |
| Max speed in low height, km/h | 469 |
| Rate of climb, m/min | 526 |
| Service ceiling, m | 10.500 |
| Range, km | 1.900 |
| Combat range, km | - |
| ARMAMENT | Two 20 mm cannons ShVAK and five 7,62 mm machine-gun ShKAS. Warload-max 2.000, normal 1.000 kg. Possibility of transport 10 rockets RS-132. |
