Mil Mi-6
Development of the Russian Mi-6 (NATO Designation: 'Hook') heavy transport helicopter began in 1952; production took off in 1957. Under extreme circumstances, the cargo cabin can hold up to 150 people; in the ambulance version, 41 stretchers and 2 seats. Normally, the passenger cabin can accommodate 61 passengers. Maximum internal and slung payloads are 12,000 kg and 8,000 kg, respectively.
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Compound type: Lift
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 5-6
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Overall Dimensions
Data on aircraft sizeOverall Height: 9.86 m (32.3 ft)
Overall Length: 41.74 m (136.9 ft)
Overall Width: 35.00 m (114.8 ft)
Engine Details
Aircraft powerplant (lift and/or propulsion)Total number of engines: 2
Engine designation: Soloviev D-25V turbine
Engine manufacturer: Soloviev Design Bureau
Take-off / rated power: 4103 kW (5500 hp)
Weights and Performance
Data on aircraft weight and flight characteristicsMax Gross Weight (ground): 41700 kg (91933 lb)
Max Range: 500 km (270 nm)
Max Endurance: 3.0 hrs (3.0 hrs)
