Attribute | ![]() Agusta Westland AW101 VVIP × | ![]() Mil Mi-8 “Hip” × |
---|---|---|
General | ||
Manufacturer | AgustaWestland | MIL Helicopters |
Model | Agusta Westland AW101 VVIP | Mil Mi-8 “Hip” |
Country | United Kingdom | Russia |
Manufactured from (year) | 1990 | 1961 |
Type | Large Helicopters | Military Helicopters |
Icao | EH10 | - |
Performance | ||
Engine | 3x 3 x Rolls Royce RTM322-01 | 2 × Klimov TV3-117Mt turboshafts - |
Power, hp (hp) | 2,100 | 1,950 |
Avionics | NVG compatible glass cockpit | - |
Max cruise speed (km/h) | 309 | 224 |
Travel range (km) | 1,389 | 959 |
Fuel economy (km/l) | 0.264 | 0.298 |
Service ceiling (m) | 4,572 | 4,500 |
Rate of climb (m/sec) | 10.16 | 8.99 |
Weights | ||
Max take off weight (kg) | 15,600 | 12,000 |
Max payload (kg) | 5,443 | 3,000 |
Fuel tank capacity (l) | 5,224 | 3,702 |
Baggage volume (m³) | 28.3 | - |
Dimensions | ||
Seats | 24 | 28 |
Cabin height (m) | 1.83 | 1.26 |
Cabin width (m) | 2.49 | 1.2 |
Cabin length (m) | 6.5 | - |
Exterior length (m) | 22.8 | 18.17 |
Tail height (m) | 6.65 | - |
Fuselage diameter (m) | 2.8 | - |
Wing span (m) | 18.6 | 21.29 |
Wing tips | No Winglets | No Winglets |