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 .Mil Moscow Helicopter Plant Wikipedia link

Mil Moscow Helicopter Plant (‹See Tfd›Russian: Московский вертолётный завод им. М. Л. Миля) is a Russian, and formerly Soviet, designer and producer of helicopters headquartered in Tomilino. It is a subsidiary of Russian Helicopters. The Moscow Mil Helicopter Plant includes a design bureau and an experimental production plant. The Mil Design Bureau is one of the world's leading developers of helicopters, with particular expertise in heavy-lift helicopters. It has developed both civil and military versions in a wide range of payload capacities, including the world's largest in serial production, 

Amazing Mil Moscow Helicopter Plant.

Mil was established in 1947 under the guidance of Mikhail Mil as the helicopter laboratory of the Central Aerohydrodynamic Institute in Zhukovsky, Moscow Oblast. The Mil Mi-1 became the first mass-produced Soviet helicopter. The Mi-8 helicopter, designed in the early 1960s, was a successful design in both military and civil applications, with over 12,000 units being produced. Mil merged with Kamov and Rostvertol to form Russian Helicopters in 2006. The Mil brand name has been retained, although the new company eliminated overlapping product lines.

Kaman Helicopters

Types

Mil Mi-1
MIL Mi-4 HOUND
EMERCOM Mi-26T
  • Mil Mi-1, 1948 - Light multi purpose helicopter. NATO reporting name Hare.
  • Mil Mi-2, 1965 - Light multi purpose helicopter. NATO reporting Name Hoplite.
  • Mil Mi-3 (1954), 1954 - Mi-1 with four-blade rotor
  • Mil Mi-3, 1964 - experimental light-utility helicopter developed from the Mi-2
  • Mil Mi-4, 1955 - Transport and submarine-hunting-helicopter. NATO reporting name Hound.
  • Mil V-5, 1959 - medium single-turboshaft transport helicopter
  • Mil Mi-6, 1957 - Heavy transportation helicopter. NATO reporting name Hook.
  • Mil V-7, 1959 - experimental four-seat helicopter
  • Mil Mi-8, 1961 - Multi-purpose helicopter. NATO reporting name Hip.
  • Mil Mi-9, airborne command post and relay variant of Mi-8
  • Mil Mi-10, 1962-1963 - Skycrane. NATO reporting name Harke.
  • Mil V-12 (1951), 1951 - designation for Mi-4 prototype.
  • Mil V-12, 1967 - experimental heavylift helicopter, 2 prototypes built, world's largest helicopter ever. NATO reporting name Homer.
  • Mil Mi-14, 1978 - Anti-submarine warfare helicopter. NATO reporting name Haze.
  • Mil V-16, 1967 - heavy cargo/transport helicopter project
  • Mil Mi-17, 1974 - Transportation helicopter. NATO reporting name Hip-H. Known as Mi-8M in Russia.

  • Full List read more in Wikipedia

Created in 1947


Company type Joint-stock company
Industry Aerospace
Founded 1947; 77 years ago
Founder Mikhail Mil
Headquarters Tomilino, Russia
Revenue $184 million (2017)
Operating income $21.5 million (2017; 2011)
Net income $6.79 million (2017)
Total assets $287 million (2017)
Total equity $69.1 million (2017)
Parent Russian Helicopters
Website https://www.rhc.
aero/structure/nhc

Helicopters Mil Moscow Helicopter Plant is an Russian aerospace company.

Mil Moscow Helicopter Plant : Commercial & Military Helicopters.

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Famous  Mil Mi  Helicopters.

Amazing Mil Moscow Helicopter Plant is an Russian aerospace company, with headquarters in Tomilino, Russia.

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Mil Mi Logo

Mikhail Leontyevich Mil  was the founder and general designer of the Mil Moscow Helicopter Plant

Mil Mi-1 Hare

Mil Mi-1 (USAF/DoD reporting name "Type 32",[2] NATO reporting name "Hare"

Mil Mi-4 Hound

Mil Mi-4 (USAF/DoD reporting name "Type 36",[1] NATO reporting name "Hound")

Mil Mi-24 Hind

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Mil Mi-28 Havoc

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Mil V-12 Hoomer

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Mil Moscow Helicopter Plant is an Russian aerospace company, with headquarters in Tomilino, Russia. 

Mil Moscow Helicopter Plant is an Russian aerospace company, with headquarters in Tomilino, Russia.
The Mil Mi-1 (USAF/DoD reporting name "Type 32", NATO reporting name "Hare

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Mil Mi-1 type 32 "Hare"

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General characteristics

  • Crew: 1
  • Capacity: 3 passengers
  • Length: 12.10 m (39 ft 8 in) (fuselage length), 17.00 m (55 ft 9 in) (overall length)
  • Height: 3.30 m (10 ft 10 in)
  • Airfoil: NACA 230 (rotor blades)
  • Empty weight: 1,760 kg (3,880 lb)
  • Max takeoff weight: 2,460 kg (5,423 lb)
  • Fuel capacity: 240 L (63 US gal; 53 imp gal)
  • Powerplant: 1 × Ivchenko AI-26V seven-cylinder air-cooled radial engine, 429 kW (575 hp)
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Performance

    • Maximum speed: 170 km/h (110 mph, 92 kn) at sea level
    • Range: 600 km (370 mi, 320 nmi)
    • Service ceiling: 3,000 m (9,800 ft)
    • Rate of climb: 5.30 m/s (1,043 ft/min)
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