Mi-24 (Export version Mi-35) attack/transport and gunship helicopter is conventionaly designed with a five blade main rotor and three blade tail rotor. Two turboshaft engines are mounted above fuselage midsection. The body of helicopter has short weapons carrying wings mounted at the body midsection. The tricycle landing gear has retractable nose-wheel. Depending on version, helicopter can carry machine guns, antitank misiles, rockets and grenade launchers.
The two crew (pilot and weapons operator) are seated in tandem armoured cockpits. The main cabin can accommodate eight persons or four stretchers. More than 2,500 have been produced and Mi-24 is in service in 34 countries.
Technical Data
Rotor diameter | Main 17,3 m |
Tail 3,9 m | |
Wing Span | 6,5 m |
Length | 17,5 m (fuselage) |
Height | 6,5 m |
Weight | Maximum 11 500 kg |
Takeoff 11 100 kg | |
Empty 8 500 kg | |
Maximum Speed | 335 km/h |
Cruising Speed | 295 km/h |
Range | Normal Load 450 km |
With Aux.Fuel 950 km | |
Service Ceiling | 4 500 m |
Vertical Climb Rate | 15 m/s |
We offer
- Logistic Support
- Spare Parts and Systems Supply, Technical Assistance
- Full Mission Simulators, Test benches, Diagnostics
- Airframe & Engine and its components Repairs & Overhauls, Technology Supplies
- Training of Pilots and Grand Personnel
- Helicopter Systems Upgrading, Conversions, Armour Plating, Extra Fuel Tanks
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