The helicopter is used to increase the mobility of land force troops, tactical airborne assault, as well as for defeat of opponent forces by unguided missiles, small arms and bombing armament.
Modification |
Mi-8MT |
Diameter of the main rotor, m |
21.30 |
Diameter of anti-torque rotor, m |
3.91 |
Length, m |
18.42 |
Height, m |
5.34 |
Weight, m: |
|
- empty |
7200 |
- Normal takeoff |
11100 |
- Maximum takeoff |
13000 |
Type of engine |
2 GTD Klimov TV3-117 |
Power, kilowatt |
2 х 1454 |
Maximum speed, km/h |
250 |
Cruising speed, km/h |
230 |
Practical range, km |
500 |
Rate of climb, m/min |
540 |
Practical limit, m |
5000 |
Static limit, m |
1760 |
Crew, per |
2-3 |
Pay load: |
Up to 24 passengers or 12 stretchers with entourage or 4000 kg of cargo in cab or 4000 kg on suspension |