The helicopter air-borne armament system includes
Takeoff weight, kg: normal maximum |
10 400 10 800 |
Maximum speed , km/h | 300 |
Cruise speed, km/h | 260 |
Flight range (internal fuel tanks), km | 460 |
Operating ceiling, m | 5 500 |
Static ceiling, exclusive of ground effect, m | 4 000 |
Maximum climbing capacity, m/s | 16 |
Crew size, persons | 2 |
Helicopter dimensions, m: length (inclusive of the rotor) width (inclusive of the gear) height (when stored) |
15.86 4.611 5.01 |
Engines: type |
VK-2500 or VK-2500P |