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Mil Mi 2

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Top speed
  
200 km/h

Wingspan
  
14 m

Engine type
  
Klimov GTD-350

Length
  
11 m

Introduced
  
1965

First flight
  
September 22, 1961

Mil Mi-2 Mil Mi2 Specifications Technical Data Description

Manufacturers
  
PZL, Mil Moscow Helicopter Plant, PZL-Świdnik

Mil mi 2 take off


The Mil Mi-2 (NATO reporting name Hoplite) is a small, lightly armored turbine-powered transport helicopter that could also provide close air support when armed with 57 mm rockets and a 23 mm cannon.

Contents

Mil Mi-2 Mil Mi2 helicopter development history photos technical data

Moldaeroservice mil mi 2 engine start up departure landing from b l i airport moldova


Design and development

The Mi-2 was produced exclusively in Poland, in the WSK "PZL-Świdnik" factory in Świdnik.

Mil Mi-2 httpsuploadwikimediaorgwikipediacommonsthu

The first production helicopter in the Soviet Union was the Mil Mi-1, modelled along the lines of the S-51 and Bristol Sycamore and flown by Mikhail Mil's bureau in September 1948. During the 1950s it became evident, and confirmed by American and French development, that helicopters could be greatly improved with turbine engines. S. P. Isotov developed the GTD-350 engine and Mil used two of these in the far superior Mi-2.

Mil Mi-2 1000 images about Mil Mi2 on Pinterest Models Armed forces and

The twin shaft-turbine engines used in the Mi-2 develop 40% more power than the Mi-1's piston engines, for barely half the engine weight, with the result that the payload was more than doubled. The Mi-2 fuselage was extensively altered from its predecessor, with the engines mounted overhead. However, the external dimensions remained similar.

Mil Mi-2 FileMil Mi2 Hoplite 7964796014jpg Wikimedia Commons

The Mil-built prototype first flew in the Soviet Union on 22 September 1961, after the initial development the project was transferred to Poland in 1964. The first Świdnik-built example flew on 4 November 1965 (making this the only Soviet-designed helicopter to be built solely outside the Soviet Union). PZL-Świdnik produced a total of 5,497 helicopters, about a third for military users. The factory also developed fiberglass rotor blades, and developed the wide-body Mi-2M seating 10 passengers instead of eight. Most typical kits include four stretchers for air ambulance usage, or aerospraying or cropdusting applications.

Mil Mi-2 Two39s Complement Flying on an Antonov AN2 and a Mil MI2

In Poland, there were also developed several specialized military variants for support or reconnaissance roles, with 23 mm autocannon, machine guns and/or two 57 mm rocket pods, four 9K11 Malyutka anti-tank missiles or Strela-2 AA missiles.

Operational history

Mil Mi-2 FileBarkol Mil Mi2jpg Wikimedia Commons

The Mi-2 was first introduced into the Soviet Air Force in 1965. The Mi-2 is used by mainly former Soviet and Eastern Bloc countries, although it was also purchased by Mexico and Myanmar armed forces.

Most of the armed Mi-2 variants were used by Poland. Some were also used by the former East Germany (with machine gun and unguided rocket armament only).

North Korea still maintains a large active fleet of Mi-2s.

Variants

V-2
First prototype.
V-2V
Armament prototype.
Mi-2 Platan
Aerial minelayer version.
Mi-2A
Mi-2B
Upgraded export version for the Middle East, fitted with improved systems and navigational aids.
Mi-2Ch Chekla
Chemical reconnaissance / smokescreen layer version.
Mi-2D Przetacznik
Aerial command post equipped with R-111 radio.
Mi-2FM
Survey version.
Mi-2P
Passenger / cargo version, with accommodation for 6 passengers.
Mi-2R
Agricultural version.
Mi-2RL
Land rescue/ambulance version.
Mi-2RM
Sea rescue version equipped with electric winch for two people and dropped rafts.
Mi-2Ro
Reconnaissance version equipped with cameras.
UMi-2Ro
Reconnaissance trainer version.
Mi-2RS Padalec ('Slowworm')
Chemical and biohazard reconnaissance version.
Mi-2S
Air ambulance version, equipped to carry four litters, plus an attendant.
Mi-2Sz
Dual-control training version.
Mi-2T
Cargo/utility version.
Mi-2U
Dual-control training version.
Mi-2US
Armed version fitted with a fixed 23mm NS-23 cannon, 4 x 7,62mm PKT machine gun pods and optional cabin PK machine gun.
Mi-2URN Żmija ('Viper')
Armed reconnaissance variant armed with a fixed 23mm NS-23 gun and two 16x57mm S-5 unguided rocket pods Mars-2. Optional 7,62mm PK machine gun window-mounted.
Mi-2URP Salamandra ('Salamander')
Gunship and anti-tank variant, armed with 23mm NS-23 gun, optional window-mounted 7,62mm PK machine gun, and 4x AT-3 Sagger (9M14M Malutka) wire-guided missiles on external weapons racks and 4x additional missiles in the cargo compartment.
Mi-2URP-G Gniewosz ('Smooth snake')
Mi-2URP with additional 4x AA missiles Strzała-2 (Strela 2) in two Gad rocket launchers.
Mi-2 Plus
Upgraded Mi-2 with uprated GTD-350W2 engines, all-composite rotor blades, new avionics and other modifications.
Mi-3
Planned Mi-2 derivative that lacked suitable engines for the program to continue.
Mi-2MSB
Modernized by Motor Sich to passenger-transport version for the civil aviation.
Mi-2MSB-V
Modernized by Motor Sich for Ukrainian Air Force.

Operators

 Algeria
  • Algerian Air Force
  •  Armenia
  • Armenian Air Force
  •  Azerbaijan
  • Azerbaijani Air Force
  •  Belarus
  • Belarusian Air Force
  •  Bulgaria
  • Bulgarian Air Force
  •  Cuba
  • Cuban Air Force
  •  Czech Republic
  • Czech Air Force
  •  Djibouti
  • Djibouti Air Force
  •  Estonia
  • Estonian Air Force
  •  East Germany
  • East German Air Force
  •  Germany
  • German State Police
  •  Hungary
  • Hungarian Air Force
  • Hungarian Police
  •  Indonesia
  • Indonesian Navy
  • Indonesian Police
  •  Latvia
  • Latvian Air Force
  •  Libya
  • Libyan Air Force
  •  Lithuania
  • Lithuanian Air Force
  •  Mexico
  • Mexican Navy
  •  Mongolia
  • Mongolian Air Force
  •  Myanmar
  • Myanmar Air Force
  •  Nicaragua
  • Nicaraguan Air Force
  •  North Korea
  • North Korean Air Force
  •  Poland
  • Polish Air Force
  • Polish Army
  • Polish Border Guard
  • Polish Navy
  •  Peru
  • Peruvian Army
  •  Russia
  • Russian Army
  •  Slovakia
  • Slovak Air Force
  •  Syria
  • Syrian Air Force
  •  Ukraine
  • Ukrainian Air Force
  •  United States
  • United States Army
  • University of Iowa
  •  Soviet Union
  • Aeroflot
  • Soviet Air Force
  • Soviet Army Aviation
  •  Yugoslavia
  • Yugoslav People's Army
  • Yugoslav Air Force.
  • Specifications (Mi-2T)

    Data from Jane's All The World's Aircraft 1982–83

    General characteristics

  • Crew: One
  • Capacity: 8 passengers or 700 kg (1,543 lb) internal, 800 kg (1,764 lb) external cargo
  • Length: 11.40 m (37 ft 4¾ in)
  • Rotor diameter: 14.50 m (47 ft 6⅞ in)
  • Height: 3.75 m (12 ft 3½ in)
  • Disc area: 165.13 m² (1,777.44 ft²)
  • Empty weight: 2,372 kg (5,218 lb)
  • Loaded weight: 3,550 kg (7,826 lb)
  • Max. takeoff weight: 3,700 kg (8,157 lb)
  • Powerplant: 2 × PZL GTD-350P turboshafts, 298 kW (400 shp) each
  • Performance

  • Maximum speed: 200 km/h (108 knots, 124 mph)
  • Range: 440 km (237 nmi, 273 mi) (max internatal fuel, no reserves)
  • Service ceiling: 4,000 m (13,125 ft)
  • Rate of climb: 4.5 m/s (885 ft/min)
  • Disc loading: 22.41 kg/m² (4.59 lb/ft²)
  • Power/mass: 12.4 kg/kW (20.4 lb/hp)
  • References

    Mil Mi-2 Wikipedia