Science Fair Project Encyclopedia
Categories: International military transport aircraft 2000-2009 | International cargo aircraft 2000-2009 | Helicopters
Euromil Mi-38
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 partly Mi-6. It is being marketed in both military and civil versions.
Specifications (Mil-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: 2x 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: 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)
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
Categories: International military transport aircraft 2000-2009 | International cargo aircraft 2000-2009 | Helicopters
Last updated: 10-15-2005 22:58:13
10-26-2009 08:16:03
The contents of this article is licensed from www.wikipedia.org under the GNU Free Documentation License. Click here to see the transparent copy and copyright details
The contents of this article is licensed from www.wikipedia.org under the GNU Free Documentation License. Click here to see the transparent copy and copyright details