Mil Mi-2 helicopter

 

The Mil Mi-2 (NATO reporting name Hoplite) is a small, three rotor blade Soviet-designed multi-purpose helicopter developed by the Mil Moscow Helicopter Plant designed in the early 1960s, and produced exclusively by WSK "PZL- widnik" in Poland. Primarily designed for civilian purposes, its military application is mainly limited to reconnaissance, transport, and courier tasks. The versatility of this helicopter is demonstrated by its impeccable adaptation to all aerial tasks we provide. Our company has developed proprietary tools for this type, which we successfully apply, among other things, in aerial agricultural work or disaster management.

FEATURES:

  • Fast
  • Agile
  • Can transport 6 people in addition to the pilot
  • Payload capacity with external suspension: 800 kg

 

FLIGHT CHARACTERISTICS:
Max. speed: 220 km/h
Range: 340 km
Maximum flight altitude: 4000 m
Rate of climb: 4,5 m/s

 

DIMENSIONS:
Length: 11,90 meters
Height: 3,70 meters
Rotor diameter: 14,60 meters

 

WEIGHT DATA:
Empty weight: 2372 kg
Max. takeoff weight: 3700 kg

 

POWERPLANT:
Type: 2 x PZL GTD–350 turboshaft engines, 300 kW (400 shp) each
Performance 2x298 kW

 

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