Mil Mi-8

Origin: Soviet Union / Russia
Prototype: maiden flight July 7, 1961
History:
  • produced since 1961
  • NATO reporting name : „Hip“
  • transport, assault transport, medicine, mine laying, artillery observation, photoreconnaissance, fuel transport, etc. helicopter
Crew: 3 – two pilots and flight engineer
Powerplant: 2 x Klimov TV2-117 turboshafts á 1,105 kW, fuel consumption 600 kg/h
Performance:
  • capacity: 24 passangers or 3 t or 12 stretshers
  • max speed 250 km/h
  • range 450 km/h, ferry range 960 km
  • service ceiling 4,500 m
  • rate of climb 9 m/s
Weight: empty weight 6.99 t, max takeoff weight 12 t
Dimensions: length 18.2 m, rotor diameter 21.29 m, height 5.65 m; disc area 356 m2
Armament: rockets and anti-tank missiles
Versions: many versions: navy Mi-14, attack helicopter Mi-24/35, and   thoroughly modernised Mi-17; Number built 17,000 +
Operators: Russia + 80 other states

https://en.wikipedia.org/wiki/Mil_Mi-8