MIL MI 24 ‘HIND’

 

ORIGIN:

Union of Soviet Socialist Republics

TYPE:

Two-seat armoured transport and attack helicopter

ENGINE:

[Mi 24D]

Two 1,641 kw (2,200 shp) Klimov [Isotov] TV3-117 Series III turboshafts

SPECIFICATIONS:

  • Wingspan: 6.536 m (21 ft 5½ in)
  • Length overall: 19.79 m (64 ft 11 in)
  • Height: 6.50 m (21 ft 4 in)
  • Main rotor diameter: 17.30 m (56 ft 9 in)
  • Max speed (clean): 310 km/h (192 mph)
  • Max cruising speed: 260 km/h (162 mph)
  • Max rate of climb at sea level: 750 m/min (2,461 ft/min)
  • Service ceiling: 4,500 m (14,765 ft)
  • Hovering ceiling out of ground effect: 2,200 m (7,220 ft)
  • Range on internal fuel: 750 km (466 miles)
  • Empty weight: 8,400 kg (18,519 lb)
  • Loaded weight: 12,500 kg (27,557 lb)

PHOTO SOURCE:

https://en.wikipedia.org/wiki/Mil_Mi-24#/media/File:Mi24CP_(modified).jpg

Categories

M