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
Engine Class Top Speed (km/h) Maximum Mass (kg) Connections
Exemplifies
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)PlatformsQuote, 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 bureauQuote, 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 Source2. 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-Ĺwidnik produced a total of 5,497 helicopters, about a third for military users.
View the SourceMil Moscow Helicopter Plant (GlobalSecurity.org)
PlatformsQuote, 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.
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