Transport Atlas

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Mil Mi-2

Lighter-Than-Air Craft and Rotorcraft

The Mil Mi-2, NATO reporting name Hoplite, is a light twin-turbine multipurpose helicopter designed by the Mil Design Bureau in the Soviet Union to replace the piston-engined Mi-1. The first prototype flew in September 1961. It is a single-pilot machine with a three-bladed main rotor and a two-bladed tail rotor, and it carries up to eight passengers, light freight, or two stretchers with an attendant, and it can also be fitted with rocket pods, gun pods, mine dispensers or a smoke generator. After a 1964 agreement, development and series production passed to Poland, where the PZL company at Swidnik began building it two years later. Several thousand were produced, and by 2005 more than 1,500 were still flying in many parts of the world.

Facts
Year
1961 1
Engine Class
Turboshaft 1
Status
Out of production 1
Units Built
5497 2
Top Speed (km/h)
200 2
Mass (kg)
2372 2
Maximum Mass (kg)
3700 2
Comparison
Body Style
Helicopter 1
Connections

Exemplifies

Aviation, Modes
Source Mil Mi-2 Hoplite (GlobalSecurity.org)

Of Make

Source Mil Moscow Helicopter Plant (GlobalSecurity.org)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Mil Moscow Helicopter Plant (GlobalSecurity.org)Platforms
Quote, Platforms
MiL has developed and put into mass production 12 major platforms, being the Mi-1, Mi-2, Mi-4, Mi-6, Mi-8, Mi-10, Mi-10K, Mi-14, Mi-17, Mi-24, Mi-26 and Mi-34.

Originated In

Also in Geography Atlas: where this subject originated.

Source Mil Mi-2 Hoplite (GlobalSecurity.org)Introduction, design bureau
Quote, Introduction, design bureau
The Mi-2 is a single pilot, light transport type helicopter designed by the Mil Design Bureau of the former USSR and built in Poland by WSK-PZL Swidnik.
Sources
1. Mil Mi-2 Hoplite (GlobalSecurity.org)
  • Introduction
    Mil Mi-2 is a light multi-purpose twin-turbine engine helicopter.
  • Description of the engines
    Two turboshaft enginess are mounted side-by-side on top of cabin, forming a hump
  • Development, first flight
    The first prototype of Mi-2 (NATO reporting name Hoplite) flew in September 1961.
  • Development, production
    Several thousand of these aircraft were built and it remained in production until 1985.
  • Introduction, design bureau
    The Mi-2 is a single pilot, light transport type helicopter designed by the Mil Design Bureau of the former USSR and built in Poland by WSK-PZL Swidnik.
View the Source
2. Mil Mi-2 (Wikipedia)
  • Specifications, empty weight
    Empty weight: 2,372 kg (5,229 lb)
  • Specifications, maximum take-off weight
    Max takeoff weight: 3,700 kg (8,157 lb)
  • Specifications, maximum speed
    Maximum speed: 200 km/h (120 mph, 110 kn)
  • Design and development, production
    PZL-Świdnik produced a total of 5,497 helicopters, about a third for military users.
View the Source
Mil Moscow Helicopter Plant (GlobalSecurity.org)
Platforms
Quote, Platforms
MiL has developed and put into mass production 12 major platforms, being the Mi-1, Mi-2, Mi-4, Mi-6, Mi-8, Mi-10, Mi-10K, Mi-14, Mi-17, Mi-24, Mi-26 and Mi-34.
View the Source
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