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  • Mil Mi-2 Hoplite




    The Mi-2, NATO code name 'Hoplite', was developed in the early 1960's by the Mil bureau as a turbine-powered version of the Mi-1 Hare. The recently development of the shaft-turbine engine revolutionized the design of the helicopter. The twin turbines develop 40% more power than the Mi-1's piston engine for barely half the dry weight, more than doubling the payload. The fuselage of the Mi-2 greatly differs from that of the Mi-1, carrying the engines above the cabin but the overall dimensions of the two models remain closely similar.

    The Mi-2 was flown in 1962, but never put into production in the Soviet Union. Instead responsibility for the type was assigned to WSK-Swidnik (now PZL) to Poland as part of a eastern europe Comecon rationalization programme, becoming the only Soviet-designed helicopter to be built solely outside the Soviet Union. Production in Poland started in 1965 and in by 1990s, PZL factory introduces a new variant: the W-3.

    Mi-2 view blueprint


    The following Mi-2 is preserved at Museo Aeronautico "Estancia Santa Romana" in San Luis, Argentina

    Mi-2

    Mi-2

    Mi-2 helilcopter plate


    Specifications

    8 passenger utility helicopter Rotor diameter: 14.56 m
    Length: 12 m
    Height: 3.75 m
    Disc area: 160 m2

    Weights: empty: 2370 kgs, Max: 3700 Kgs, slung load: 800 kgs.

    Engine: 2 Isotov GTD-350 of 431 shp

    Speed: Max: 210 km/h
    Range: 340 km
    Service Ceiling: 4000 m


    Mi-2 cockpit





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