In numbers Through the lens Video
NATO reporting name: Blinder
Technical specifications
| DESIGNER | OKB Tupolev |
| COUNTRY | Russia |
| TYPE |
Supersonic βomber
|
| CREW |
3
|
| POWER-PLANT | Two turbojet engines VD-7M |
| Thrust, kgf | 2x16.000 |
|
DIMENSIONS
|
|
|
Length, m
|
41,60 |
|
Height, m
|
10,13 |
|
Wing span, m
|
23,17 |
|
Wing area, m2
|
162,25 |
| WEIGHT | |
| Maximum take-off, kg | 85.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | - |
| Internal fuel, l (kg) | - |
| Warload, kg | |
| - in standard configuration | 9.000 |
| - maximum | 12.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 1.510 |
| Cruising speed, km/h | - |
| Range, km | 5.850 |
| Combat range, km | 3.150 |
| Service ceiling, m | 14.700 |
| Runway, m | - |
| Maximum overload, g | - |
| ARMAMENT | Permanent armament consists of a 23 mm NR-23 gun, which is located directly above the engine nozzles. Bomb transport standard configuration 24 FAB-500 or one FAB-9000. |