Euromil Mi-38
From Wikipedia, the free encyclopedia
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.
[edit] Specifications (Mi-38)
[edit] 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: 2×Pratt & Whitney Canada PW127 turboshafts, 1,865 kW (2,500 shp) each
[edit] Performance
- Maximum speed: 275 km/h (171 mph)
- Range: 1,300 km (811 miles)
- Service ceiling: 6,500 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)
[edit] External links
[edit] 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
[edit] 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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