In numbers Through the lens Video
Three-view drawing
Technical specifications
| DESIGNER | OKB Sukhoi |
| COUNTRY | Russia |
| TYPE |
Strategical bomber
|
| CREW | 3 |
| POWER-PLANT | Four turbofan engines with afterburning type RD-36-41 (ΝΚ-101) |
| Thrust, kgf | 4x16.000 (4x20.000) |
| DIMENSIONS | |
| Length, m | 41,70 (42,20) |
| Height, m | 8,00 |
| Wing span, m | 14,14 |
|
- with a sweep angle of 30 degrees
|
40,8
|
|
Wing area, m2
|
97,5
|
|
Wing area, m2 (with a sweep angle of 30 degrees)
|
40,80
|
| WEIGHT | |
| Maximum take-off, kg | 170.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 90.000 |
| Internal fuel, kg | - |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 3.200 |
| Maximum speed in low height, km/h | 1.100 |
| Cruising speed, km/h | - |
| Service ceiling, m | 24.000 |
|
Maximum range at cruising speed
with normal weapons load without aerial refueling, km: |
|
|
- at a speed of 900 km/h
|
11.000 / 14.000
|
|
- at a speed of 3.000 km/h
|
7.500 / 9.000
|
|
Take-off distance, m
|
1.350 / 1.100
|
|
Landing distance, m
|
950
|
| Combat range, km | - |
| Maximum overload, g | - |
| ARMAMENT |
It can carry 2-4 Kh-45, 24 Kh-2,000 air-to-surface missiles.
|