MIL Mi 34

 

ORIGIN:

Russia

TYPE:

light utility helicopter

ENGINE:

One 240 kw (320 hp) Vedeneyev M-14V-26V nine-cylinder, air-cooled radial engine

SPECIFICATIONS:

  • Main rotor diameter: 10.01 m (32 ft 10 in)
  • Length, rotors turning: 11.42 m (37 ft 6 in)
  • Fuselage length: 8.75 m (28 ft 9 in)
  • Height: 2.75 m (9 ft 0 in)
  • Main rotor disc area: 78.5 m² (845 sq ft)
  • Max speed: 225 km/h (140 mph)
  • Max cruising speed: 180 km/h (112 mph)
  • Normal cruising speed: 160 km/h (99 mph)
  • Service ceiling: 4,999 m (16,400 ft)
  • Hovering ceiling: 1,500 m (4,920 ft)
  • Range with max fuel with 245 kg (540 lb) payload: 420 km (261 miles)
  • Endurance at cruising speed: 2 hrs 26 mins
  • Empty weight: 950 kg (2,094 lb)
  • Loaded weight: 1,450 kg (3,196 lb)

PHOTO SOURCE:

https://pl.wikipedia.org/wiki/Mi-34#/media/Plik:Mil_Mi-34S_Hermit.jpg

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