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Military


Mi-6 HOOK (MIL)

Specifications
Country of Origin Russia
Builder Mil
RoleHeavy transport (65 equipped troops), vehicles
Similar AircraftMi-26 Halo, CH-3 Jolly Green Giant
Rotor diameter 115 ft (35 m)
Length 109 ft (33.3 m)
Height 
Mass M-6 Mid- 6P
Empty weight 27,240 kg kg 27,000 kg
Mass normal of fuel 6,315 kg
Mass fuel with tanks ext. 9,805 kg
Maximum fuel mass (convoying) 13.295 kg
Maximum payload 12,000 kg 12,360 kg
External maximum loading under sling 9000 kg
Mass normal on takeoff 40,500 kg 40,500 kg
Maximum mass on takeoff 42,500 kg 42,500 kg
Max. mass with max. load under sling with less than 1000 m of altitude. 37,500 kg
EngineTwo turbomotors Soloviev D-25B (TB-2BM) developing each one 4100 kw with takeoff and 3505 kw of nominal nominal output
Maximum speed300 km/h
Cruising speed250 km/h
Dynamic ceiling in condition ISA at maximum mass 4,400 meters
Dynamic ceiling in condition ISA, + 30C at maximum mass 3,300 meters
Dynamic ceiling in condition ISA with the mass of 32,000 kg 6,750 meters
Dynamic ceiling in condition ISA, + 30C with mass of 32,000 kg 6,000 meters
Static ceiling at 40,000 kg, in condition ISA 2,500 meters
Static ceiling at 40,000 kg, in condition ISA + 15 C 2,000 meters
Static ceiling at 32,000 kg, in condition ISA 4,500 meters
Static ceiling at 32.000 kg, in condition ISA + 30C 3,500 meters
Range 12,000 kg of load, principaltanks only and 5% of reserves 200 km
Range with 9.000 kg of load, principal tanks only and 5% of reserves 550 km
Maximum Range with external tanks, 4,000 kg load and 5% fuel reserve 1,000 km
Range with normal takeoff mass, with 10.000 kg of load, principal tanks only, 5% fuel reserves 225 km
Maximum Range with takeoff normal mass, with external tanks, 2,000 kg load and 5% fuel reserves 1,050 km
Maximum Ferry Range 1,450 km
Armament Machine gun
Crew Five
Cost 
User Countries Algeria, CIS, Egypt, Iraq, Laos, Peru, Syria, Vietnam

Types Mi-6 Mi-6A Mi-6PZh
Year of first flight 1957 1971 1967
Crew 5 5 5
Passengers 61 65 - 90 61
Powerplant D-25V D-25V D-25V
Take-off power, hp 2 5500 2 5500 2 5500
Main rotor diameter, m 35 35 35
Empty weight, kg 26500 27240 28724
Take-off weight, kg:
      normal 39700 40500 40500
      maximum 41700 44000 42500
Payload, kg:
      normal internal 6000 8000 6000
      maximum internal 12000 12000 12000
      external 8000 9000 3000
Speed, km/h:
      maximum 250 304 300
      cruising 200 250 250
Hovering ceiling in ground effect, mTD> 2250 2250 -
Service ceiling, m: 4500 4500 4500
Operational range, km 500 620 555




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