Mi-8 HIP
Specifications | |
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Country of Origin | Russia |
Builder | Mil |
Date of Introduction | 1967 |
Role | Armed assault-transport |
Similar Aircraft | Puma, Mi-2 Hoplite, Super Frelon |
Blades |
Main rotor: 5 Tail rotor: 3 |
Rotor diameter |
Main Rotor : 21.3 meters [70 ft] Tail Rotor : 3.9 meters |
Length |
Length (rotors turning): 25.2 m Length (fuselage): 18.2m [61 ft] |
Height | 18 ft 6 in ( 5.65 m) |
Width | 2.5 m |
Cargo Compartment |
Floor Length: 5.3 m Width: 2.3 m Height: 1.8 m |
Weight |
Maximum Gross: 12,000 kg Normal Takeoff: 11,100 kg Empty: 6,990 kg |
Engine | 2 TV2-117, 1482 hp each |
Maximum speed | 230-250 km/h |
Cruising speed | 122 kts (140 mph; 225 km/h) |
Range |
Maximum Load: 350 km Normal Load: 460 km With Aux Fuel: 950 km |
Fuel |
Internal: 445 liters Internal Aux Tank: 915 liters ea. External Fuel Tank: 745 liters in port tank, 680 liters in starboard tank |
Service Ceiling | Service: 4,500 meters Hover (out of ground effect): 800 meters Hover (in ground effect): 1,900 meters |
Vertical Climb Rate | 9 m/s |
Standard Payload |
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Armament |
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Survivability/Countermeasures |
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AVIONICS | The Mi-8 is equipped with instruments and avionics allowing operation in day, night, and instrument meteorological conditions. |
Crew | 3 (2x pilots, 1x flight engineer) |
Cost |
$900,000 (1991 used) $3,200,000 (new) |
User Countries | At least 54 countries -- Armenia, Azerbaijan, Afghanistan, Algeria, Angola, Belarus, Bulgaria, Cambodia, CIS, Croatia, Cuba, Czech Republic, Egypt, Germany, Guyana, Hungary, Iran, Iraq, Madagascar, Mongolia, Mozambique, Nicaragua, North Yemen, People's Republic of China, Slovakia, SouthYemen, Sudan, Syria, Ukraine, Vietnam, Yugoslavia, Zambia |
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