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The Mil Mi-2
Mi-2 (NATO reporting name is "Hoplite") was a small, lightly armored transport helicopter that could also provide close air support when armed with 57 mm rockets and a 23 mm cannon. It was first introduced into the Soviet Air Force in 1965. The Mi-2 was produced exclusively in Poland, with production ending in 1985.
The Mi-2 is used by mainly former Soviet countries, although it is used by Germany and Myanmar as well.
General Characteristics Crew: one, pilot Capacity: 8 troops or 700 kg (1,540 lb) internal, 800 kg (1,760 lb) external cargo Length: 11.9 m (39 ft 4 in) Main rotor diameter: 14.6 m (47 ft 11 in) Height: 3.7 m (12 ft 2 in) Main rotor area: 167 m? (1,797 ft) Empty: 2,372 kg (5,218 lb) Loaded: 3,550 kg (7,810 lb) Maximum takeoff: 3,700 kg (8,140 lb) Powerplant: 2x PZL GTD-350 turboshaft engines, 298 kW (400 shp) eac
Performance Maximum speed: 220 km/h (138 mph) Range: 340 km (212 miles) Service ceiling: 4,000 m (13,120 ft) Rate of climb: 270 m/min (886 ft/min) Main rotor loading: 21 kg/m? (4.3 lb/ft?) Power/Mass: 0.17 kW/kg (0.10 hp/lb)