Mil Mi-1
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The Mil Mi-1 (originally known to US intelligence as the Type-32 and later by the NATO reporting name Hare) was a Soviet three-seat light utility helicopter. It is powered by one 575 hp Ivchenko AI-26V radial. It entered service in 1950 and was first seen on the 1951 Soviet Aviation Day, Tushino and has since been produced for 16 years. 1,594 helicopters were built.
[edit] Specifications (Mil-1)
General characteristics
- Crew: One
- Capacity: 2 passengers or 255 kg (561 lb) of cargo
- Length: 12.09 m (39 ft 8 in)
- Rotor diameter: 14.35 m (47 ft 1 in)
- Height: 3.30 m (10 ft 10 in)
- Disc area: 161.7 m² (1,740 ft²)
- Empty weight: 1,700 kg (3,740 lb)
- Loaded weight: 2,140 kg (4,708 lb)
- Max takeoff weight: 2,330 kg (5,126 lb)
- Powerplant: 1× Ivchenko AI-26V radial engine, 429 kW (575 hp)
Performance
- Maximum speed: 185 km/h (115 mph)
- Range: 430 km (268 miles)
- Service ceiling: 3,500 m (11,480 ft)
- Rate of climb: 5.3 m/s (1,043 ft/min)
- Disc loading: 13 kg/m² (3 lb/ft²)
- Power/mass: 0.20 kW/kg (0.12 hp/lb)
[edit] Operators
Afghanistan: 12 acquired from 1957 and withdrawn from service by 1976[1].
Albania: 3 in service from 1957 through 1960[1].
Algeria
Bulgaria
China
Cuba
Czechoslovakia
East Germany
Egypt
Finland
Hungary
Iraq
Mongolia
DPR Korea
Poland
Romania
Soviet Union
Syria
[edit] References
- ^ a b "Historical Listings", [World Air Forces].
[edit] Related content
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Designation sequence
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