Technical specifications
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TECHNICAL SPECIFICATIONS
DESIGNER | OKB Tupolev |
COUNTRY | Russia |
TYPE | Long-range Bomber |
CREW | 5 |
POWER-PLANT | Two reciprocating motor ASh-83 |
Power, h.p | 2 x 1.850 |
DIMENSIONS | |
Length, m | 14,42 |
Height, m | 4,60 |
Wing span, m | 22,06 |
Wing area, m2 | 59,05 |
WEIGHT | |
Normal take-off, kg | 13.340 |
Empty aircraft, kg | 8.316 |
Maximum take-off, kg | - |
Internal fuel, kg | - |
PERFORMANCE | |
Maximum speed, km/h | 531 |
Cruising speed, km/h | 505 |
Max speed in low height, km/h | 465 |
Rate of climb, m/min | 424 |
Service ceiling, m | 9.900 |
Range, km | 2.020 |
Combat range, km | - |
ARMAMENT | Three 12,7 mm machine-gun UBT (3x150 rounds), two 20 mm cannons ShVAK (2 x 150 rounds). Warload-4.000 kg. |