Mil Mi-54
| Mi-54 | |
|---|---|
 | |
| Mil Mi-54 mock up at MAKS 2007 Airshow | |
| Role | Civil Utility helicopter |
| National origin | Russia |
| Manufacturer | Mil |
The Mil Mi-54 was a projected twin-turbine civil utility helicopter, first announced in 1992, intended to replace the Mi-2 and the Mi-8 helicopters. It was planned to use two 574 kW Saturn/Lyulka AL-32 turboshaft engines, four-bladed main and tail rotors, and fixed tricycle-type landing gear with one nosewheel and two rear wheels on sponsons.
Specifications
General characteristics
- Crew: 1-2
- Capacity:
- 10-12 passengers
- Length: 13.13 m (43.1 ft)
- Rotor diameter: 13.5 m (44 ft)
- Height: 4.8 m (16 ft)
- Empty weight: 3,000 kg (6,600 lb)
- Loaded weight: 4,500 kg (9,900 lb)
- Max. takeoff weight: 4,700 kg (10,400 lb)
- Powerplant: 2 × Saturn/Lyulka AL-32 turboshaft, 771 shp (575 kW) each
Performance
- Maximum speed: 285 km/h (177 mph; 154 kn)
- Cruise speed: 260 km/h (160 mph; 140 kn)
- Range: 600 km (370 mi; 320 nmi)
- Service ceiling: 6,000 m (20,000 ft)
External links
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