In numbers Through the lens Video
Technical specifications
| DESIGNER | OKB Tupolev |
| COUNTRY | Russia |
| TYPE |
Long range Bomber
|
| CREW | 4 |
| POWER-PLANT | Two turbofan engines ΝΚ-22 |
| Thrust, kgf | 2x22.000 |
|
DIMENSIONS
|
|
|
Length, m
|
41,16 |
|
Height, m
|
11,15 |
|
Wing span, m
|
|
| - with sweep 20ο | 34,28 |
| - with sweep 65ο | 23,30 |
| Wing area, m2 | |
| - with sweep 20ο | 183,58 |
| - with sweep 65ο | 175,78 |
| WEIGHT | |
| Maximum take-off, kg | 126.000 |
| Normal take-off, kg | 78.000 |
| Empty aircraft, kg | - |
| Internal fuel, l | - |
| Warload, kg | |
| - in standard configuration | - |
| - maximum | 24.000 |
| PERFORMANCE | |
| Maximum speed (at high altitude, 10.000 m), km/h | 2.300 |
| Cruise speed, (with Kh-22M missiles for Tu-22M2) | 900 |
| Take-off speed, km/h | 370 |
| Landing speed, km/h | 285 |
| Range, km | - |
| Service ceiling, m | 13.300 |
| Take-off distance, m | 2.100 |
| Landing distance, m | 1.300 |
| Maximum overload, g | - |
| ARMAMENT | Permanent armament consists of a twin 23mm GSh-23 gun mounted directly above the engine nozzles. |