Technical specifications 
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TECHNICAL SPECIFICATIONS
| DESIGNER | OKB Tupolev |
| COUNTRY | Russia |
| TYPE | Long-range Bomber |
| CREW | 5 |
| POWER-PLANT | Two reciprocating motor AM-44TK |
| Power, h.p | 2 x 1.950 |
| DIMENSIONS | |
| Length, m | 14,42 |
| Height, m | 4,70 |
| Wing span, m | 22,06 |
| Wing area, m2 | 59,05 |
| WEIGHT | |
| Normal take-off, kg | 15.960 |
| Empty aircraft, kg | 9.540 |
| Maximum take-off, kg | - |
| Internal fuel, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 579 |
| Cruising speed, km/h | - |
| Max speed in low height, km/h | - |
| Rate of climb, m/min | 556 |
| Service ceiling, m | 11.000 |
| Range, km | 2.570 |
| Combat range, km | - |
| ARMAMENT | Three 12,7 mm machine-gun UBT (3x195 rounds), two 20 mm cannons ShVAK (2 x 150 rounds). Warload-4.000 kg. |
