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Mi-17 Helikopter NATO "HIP"

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    Mi-17 Helikopter NATO "HIP"



    Wikipedia:
    The Mil Mi-17 (NATO reporting name "Hip") is a Russian helicopter in production at two factories in Kazan and Ulan-Ude. It is known as the Mi-8M series in Russian service. It is a medium twin-turbine transport helicopter. There are also armed gunship versions.

    The designation Mi-17 is for export; Russian armed forces call it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor on the port side instead of the starboard side, and dust shields in front of the engine intakes. Engine cowls are shorter than on the TV2-powered Mi-8, not extending as far over the cockpit, and an opening for a bleed air valve outlet is present forward of the exhaust.

    In May 2008 licensed production of the Mi-17 started in China.

    Specifications (Mil-17-1V)

    Data from Jane's All The World's Aircraft 2003–2004

    General characteristics
    • Crew: Three – two pilots and one engineer
    • Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung.
    • Length: 18.465 m (60 ft 7 in)
    • Rotor diameter: 21.25 m (69 ft 10½ in)
    • Height: 4.76 m (15 ft 7¼ in)
    • Disc area: 356 m² (3,834 ft²)
    • Empty weight: 7,489 kg (16,510 lb)
    • Loaded weight: 11,100 kg (24,470 lb)
    • Max. takeoff weight: 13,000 kg (28,660 lb)
    • Powerplant: 2 × Klimov TV3-117VM turboshafts, 1,633 kW (2,190 shp) each

    Performance

    • Maximum speed: 250 km/h (135 knots, 155 mph)
    • Range: 465 km (251 nmi, 289 mi) (standard fuel)
    • Service ceiling: 6,000 m (19,690 ft)
    • Rate of climb: 8 m/s (1,575 ft/min)

    Armament

    • up to 1,500 kg (3,300 lb) of disposable stores on six hardpoints, including bombs, rockets, and gunpods.



    Mil Mi-17
    1981

    The Mi-17 retains the codename 'Hip-H', denoting its derivation from the Mi-8 design. First identified in 1980-81, the Mi-17 is virtually a revision of the Mi-8 design using a combination of the 'Hip' airframe but with the port-side tail rotor, and fitted with the more powerful powerplants of the Mi-14. These result in an overall improvement in performance, particularly the hovering ceiling. The type remains in current production for both civil and military use as a cargo-carrying helicopter, with secondary capability as a passenger transport capable of carrying up to 24 passengers, or 12 stretcher cases when used as an ambulace. The first export examples were delivered to Cuba in 1983, and Mi-17s are now in service in Angola, Hungary, India, North Korea, Nicaragua, Papua New Guinea, Peru and Poland, as well as the CIS.

    Mil Mi-17 helicopter - development history, photos, technical data




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