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Euromil Mi-38

From PlaneSpottingWorld, for aviation fans everywhere

The Euromil Mi-38 is a cargo helicopter designed by Mil but being developed and marketed by an international consortium. It was originally intended as a replacement for the Mi-8 and the Mi-6. It is being marketed in both military and civil versions. It flew for the first time on the 22 December 2003.

Specifications (Mi-38)

General characteristics

  • Crew: two
  • Capacity: 32 passengers or 6,000 kg (13,200 lb) of cargo
  • Length: 19.70 m (64 ft 8 in)
  • Main rotor diameter: 21.10 m (69 ft 3 in)
  • Height: 5.13 m (16 ft 10 in)
  • Main rotor area: 349.5 m² (3,762 ft²)
  • Empty: 8,300 kg (18,300 lb)
  • Loaded: 14,200 kg (31,300 lb)
  • Maximum takeoff: 15,600 kg (34,400 lb)
  • Powerplant:Pratt & Whitney Canada PW127 turboshafts, 1,865 kW (2,500 shp) each

Performance

  • Maximum speed: 275 km/h (171 mph)
  • Range: 1,300 km (811 miles)
  • Service ceiling: 61,500 m (21,320 ft)
  • Rate of climb: m/min ( ft/min)
  • Main rotor loading: 41 kg/m² (8.3 lb/ft²)
  • Power/Mass: 0.26 kW/kg (0.16 hp/lb)

External links

Related content

Related development:

Comparable aircraft: EH Industries EH101 - Sikorsky S-92

Designation sequence: Mi-34 - Mi-35 - Mi-36 - Mi-38 - Mi-40 - Mi-42 - Mi-44

References

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

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