Attribute | ![]() MIL Mi-26 × | ![]() Bell Boeing V 22 Osprey × |
---|---|---|
General | ||
Manufacturer | MIL Helicopters | Bell Helicopter |
Model | MIL Mi-26 | Bell Boeing V 22 Osprey |
Country | Russia | United States |
Manufactured from (year) | 1981 | 1988 |
Type | Large Helicopters | Tilt Rotors |
Icao | MI26 | V22 |
Performance | ||
Engine | 2x 2 × Lotarev D-136 turboshafts | 2x 2 × Rolls-Royce Allison T406 |
Power, hp (hp) | 11,400 | 6,150 |
Avionics | Groza 7A813 weather radar, Integrated PKV-26-1 flight/nav system | AN/ARC 182 VHF/UHF , etc. |
Max cruise speed (km/h) | 294 | 500 |
Approach speed (km/h) | - | 204 |
Travel range (km) | 1,952 | 1,628 |
Fuel economy (km/l) | 0.186 | 0.24 |
Service ceiling (m) | 4,602 | 7,925 |
Rate of climb (m/sec) | 7.73 | 20.83 |
Weights | ||
Max take off weight (kg) | 56,000 | 27,443 |
Max payload (kg) | 20,000 | 9,068 |
Fuel tank capacity (l) | 12,000 | 7,665 |
Baggage volume (m³) | 6.16 | - |
Dimensions | ||
Seats | 9 | 24 |
Seats - business class | 9 | - |
Seats - first class | 65 | - |
Cabin height (m) | 3.2 | 1.83 |
Cabin width (m) | 3.1 | 1.8 |
Cabin length (m) | 12.1 | 7.37 |
Exterior length (m) | 40.03 | 17.5 |
Tail height (m) | 7.95 | 5.46 |
Fuselage diameter (m) | - | 1.9 |
Wing span (m) | 32 | 14 |
Wing tips | No Winglets | No Winglets |