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General Info

Mil Helicpter plant Mil Mi-34 type 32  'Hermit'

Type Helicopter
National origin Soviet Union / Russia
Manufacturer Mil Helicopters
Status out of production
Number built 27
History
Manufactured 1986–2011
Introduction date 1993
First flight 17 November 1986
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History Mil Moscow Helicpter plant Mil Mi-34 Izdeliye 32
NATO reporting name: 'Hermit'
  • Ml Mi-34 type 32 Hermit

    Military operators

    Bosnia and Herzegovina
    Nigeria

    Variants Military

    Mil Mi-34
    • Mi-34S – four seat production model powered by a 239 kW (325 hp) Vedeneyev (VOKBM) M-14V-26V nine-cylinder, air-cooled, radial engine mounted sideways in the fuselage, and equipped with modern avionics. A few aircraft were purchased by the Moscow police.
    • Mi-34S2 "Sapsan" – turbine version of the Mi-34. It will be able to accommodate up to 4 passengers and the first deliveries are planned by the end of 2011. It will be powered by Turbomeca Arrius-2F
    • Mi-34L – proposed version powered by a 261 kW (350 hp) Textron Lycoming TIO-540J piston engine. None built.
    • Mi-34P Patrulnyi (English: patrol) – Police patrol version for Moscow Mayor Office.
    • Mi-34A – Luxury version, intended to be powered by an Allison 250-C20R turboshaft engine. None built.
    • Mi-34M1 and Mi-34M2 – Proposed twin-turbine, six-passenger versions.
    • Mi-34UT – trainer with dual control.
    • Mi-34V or Mi-34VAZ or Mi-234 – proposed version powered by two VAZ-4265 rotary piston engines.
    • Mi-44 – proposed development with TV-O-100 engine and refined aerodynamics. A mockup was built in 1987.

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Mil Moscow Helicpter plant Mil Mi-34 Izdeliye 32 NATO reporting name: 'Hermit'

Mil Moscow Helicpter plant Mil Mi-34 Izdeliye 32
NATO reporting name: 'Hermit'

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General characteristics

  • Crew: 1
  • Length: 16 m (52 ft 6 in)
  • Height: 4.93 m (16 ft 2 in)
  • Empty weight: 7,700 kg 
  • Gross weight: 9,800 kg 
  • Max takeoff weight: 10,800 kg
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Powerplant

  • Powerplant: 2 × Klimov VK-2500 turboshaft engines, (2,400 shp) each
  • Main rotor diameter: 2 × 14.5 m 
  • Main rotor area: 330.3 m2 (3,555 sq ft) contra-rotating 3-bladed main rotors
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Specifications

  • Maximum speed: 315 km/h 
  • Cruise speed: 270 km/h 
  • Never exceed speed: 350 km/h 
  • Range: 545 km (339 mi, 294 nmi)
  • Combat range: 470 km 
  • Ferry range: 1,160 km 
  • Service ceiling: 5,500 m
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Armament

        • Guns: 1 × mobile semi-rigid 30 mm Shipunov 2A42 cannon (460 rounds total, dual feeding AP or HE-Frag)
        • Hardpoints: 6 × under-wing hardpoints, plus 2 on wingtips for countermeasures or air-to-air missiles with a capacity of 2,000 k
Special Links Mil Moscow Helicpter plant Mil Mi-34 Izdeliye 32 NATO reporting name: 'Hermit'

Links to Youtube & Others

At the time of its first flight, the Mi-34 was the smallest helicopter yet designed by Mil. Despite only entering series production in 1993, the Mi-34 development story dates back to the mid 1980s, with a first flight in 1986. The Mi-34 was first exhibited to the west at the Paris Airshow in 1987 and has made a number of appearances at major airshows, including Farnborough, since that time. The Mi-34 is the first helicopter designed in a former eastern bloc country that can loop and roll. More than 60 have been delivered, with missions including pilot training,

Mil Helicpter plant
Mi-34 type 32 'Hermit'

Production of the Mi-34 began during 1993. Sporadic low rate production since.

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Youtube Link

The Mil Mi-34 (NATO reporting name: Hermit) is a light helicopter designed by the Mil Moscow Helicopter Plant in either a two or four seat configuration for utility and training.

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