Mil Mi-54
From The Right Wiki
Jump to navigationJump to search
This article has multiple issues. Please help improve it or discuss these issues on the talk page. (Learn how and when to remove these messages)
|
| Mi-54 | |
|---|---|
| File:Khokhloma helicopter.jpg | |
| 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.[1]
Specifications
Data from [2]
General characteristics
- Crew: 2
- Capacity: 10-12 passengers
- Length: 13.113 m (43 ft 0 in)
- Height: 4.8 m (15 ft 9 in)
- Empty weight: 3,000 kg (6,614 lb)
- Max takeoff weight: 4,700 kg (10,362 lb) with external cargo on the sling, 4,500 kg (9920,802 lb) with internal cargo
- Powerplant: 2 × Saturn/Lyulka AL-32 turboshaft engines, 575 kW (771 shp) each
- Main rotor diameter: 13.5 m (44 ft 3 in)
- Main rotor area: 143.16 m2 (1,541.0 sq ft)
Performance
- Maximum speed: 280 km/h (170 mph, 150 kn)
- Cruise speed: 260 km/h (160 mph, 140 kn)
- Range: 600 km (370 mi, 320 nmi)
- Service ceiling: 5,500 m (18,000 ft)
References
- ↑ "Mil Moscow Mi-54 Multirole Transport Helicopter - Aerospace Technology". www.aerospace-technology.com. Retrieved 2022-03-21.
- ↑ "Mil Moscow Mi-54 Multirole Transport Helicopter - Aerospace Technology". www.aerospace-technology.com. Retrieved 2024-05-11.
External links
Wikimedia Commons has media related to Mil Mi-54.