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Mil Mi-2

Mil Mi-2 © Karsten Palt
Photo ©: Karsten Palt


Light Utility Helicopter

The Mil Mi-2 is a twin-engined light utility helicopter developed by the Soviet manufacturer Mil OKB, today MIL Moscow helicopter plant, JSC (Russia).
Propulsion2 Turboshaft Engines
Engine ModelKlimow / Klimov GTD-350P
Engine Power (each)450 kW604 shp
Speed191 km/h103 kts
  119 mph
Service Ceiling4.000 m13.123 ft
Range159 km86 NM
99 mi.
Empty Weight2.365 kg5.214 lbs
max. Takeoff Weight3.700 kg8.157 lbs
Rotor Blades (main/tail)4/24/2
Main Rotor Diameter14,50 m47,6 ft
Tail Rotor Diameter2,70 m8,9 ft
Rotor Disc Area165,1 m²1777 ft²
Length17,42 m57,2 ft
Height3,75 m12,3 ft
First Flight09/1961
Production Statusout of production
Total Production>6500
NATO CodeHoplite
Data for (Version)Mil Mi-2
The Mil Mi-2 was produced by WSK PZL-Swidnik in Poland only.

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