Mil Mi-12
From Wikipedia, the free encyclopedia
Mi-12 Homer | |
---|---|
Mil Mi-12 | |
Type | Heavy lift helicopter |
Manufacturer | Mil Design Bureau |
Maiden flight | 10 July 1968 |
Status | Prototype only |
Primary user | Soviet Union |
Number built | 2 |
Developed from | Mil Mi-6 |
The Soviet made Mil Mi-12 (Also known as the W-12, NATO reporting name Homer) is the largest helicopter ever built.
The MI-12 feaures the only two-rotor transverse scheme ever built by Mil eliminating the need for a tail rotor. The twin engines were taken together with the rotors from the Mil Mi-6 and duplicated on the Mi-12.
Production began on the Mi-12 prototype in 1965 with the goal of lifting no less than 30,000kg, and it flew first on July 10, 1968. In February 1969, the Prototype lifted a 31,030kg payload to 2.91m. On August 6th 1969, the Mi-12 lifted 44,205kg (88,636 lb) to a height of 2,255m (7,398 feet), a world record.
Another Mi-12 with the registration number CCCP-21142 / H-833 was built and shown around Europe including at the Paris Air Show at Le Bourget in 1971. Despite this, the helicopter did not meet its design specifications and the program was cancelled with only two aircraft built.
Some sources mention a third MI-12 prototype, which crashed during testing, but this has never been confirmed by official sources.
One of the remaining Mi-12 is on display at the Monino Air Force Museum in Russia (50km east of Moscow). The other is reportedly at the Michail Leontjewitsch Mil helicopter plant in Lyubertsy-Panki near Moscow. (as of Aug. 2006)
[edit] Specifications (Mi-12)
General characteristics
- Crew: Six
- Capacity: Up to 40,000 kg of cargo
- Length: 37.00 m (121 ft 4 in)
- Rotor diameter: 2x 35.00 m (114 ft 10 in)
- Height: 12.50 m (41 ft 0 in)
- Disc area: 1,924 m² (20,700 ft²)
- Empty weight: 69,100 kg (152,020 lb)
- Loaded weight: 97,000 kg (213,400 lb)
- Max takeoff weight: 105,000 kg (231,000 lb)
- Powerplant: 4× Soloviev D-25VF turboshafts, 4,048 kW (6,497 shp) each
Performance
- Maximum speed: 260 km/h (163 mph)
- Range: 1,000 km (625 miles)
- Service ceiling: 3,500 m (11,480 ft)
- Rate of climb: m/s (ft/min)
- Disc loading: 50 kg/m² (10 lb/ft²)
- Power/mass: 0.20 kW/kg (0.12 hp/lb)
[edit] External links
[edit] Related content
Designation sequence
- VVS
Mi-8 - Mi-9 - Mi-10 - Mi-12 - Mi-14 - Mi-17 - Mi-18
- Mil
V-5 - V-7 - V-8 - V-12 - V-16
Timeline of aviation
Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines
Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft
Notable military accidents and incidents · Notable airline accidents and incidents · Famous aviation-related deaths
Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft