Attribute | ![]() Sikorsky S-70B Seahawk × | ![]() Mil Mi-24 / Mi-25 / Mi-35 × |
---|---|---|
General | ||
Manufacturer | Sikorsky Helicopter | MIL Helicopters |
Model | Sikorsky S-70B Seahawk | Mil Mi-24 / Mi-25 / Mi-35 |
Country | United States | Russia |
Manufactured from (year) | 1984 | 1972 |
Type | Military Helicopters | Military Helicopters |
Icao | H60 | - |
Performance | ||
Engine | 2x 2 X General Electric T700-GE401C | 2 × Isotov TV3-117 turbines - |
Power, hp (hp) | 1,890 | 2,200 |
Avionics | Rockwell Collins glass cockpit, BAE Systems | - |
Max cruise speed (km/h) | 270 | 294 |
Travel range (km) | 833 | 450 |
Fuel economy (km/l) | 0.333 | 0.24 |
Service ceiling (m) | 3,658 | 4,496 |
Rate of climb (m/sec) | 8.38 | 12.5 |
Weights | ||
Max take off weight (kg) | 9,927 | 12,000 |
Max payload (kg) | 2,725 | 3,500 |
Fuel tank capacity (l) | 2,249 | 2,131 |
Dimensions | ||
Seats | 12 | 11 |
Cabin height (m) | 1.3 | 1.2 |
Cabin width (m) | 1.8 | 1.46 |
Cabin length (m) | 3.2 | 2.8 |
Exterior length (m) | 19.76 | 17.5 |
Tail height (m) | 5.18 | - |
Fuselage diameter (m) | 2.1 | - |
Wing span (m) | 16.36 | 17.3 |
Wing tips | No Winglets | No Winglets |