Mil Mi-17

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Mi-17 / Mi-8M
Two Mi-17 (Mi-8MTV1) being used for the UN
Role Transport helicopter
Manufacturer Mil Moscow Helicopter Plant
Status In service
Primary users Russia
ca. 60 other countries
Produced about 12,000[1]
Developed from Mil Mi-8

The Mil Mi-17 (also known as the Mi-8M series in Russian service, NATO reporting name "Hip") is a Russian-designed helicopter currently in production at two factories in Kazan and Ulan-Ude.

Contents

[edit] Development

Developed from the basic Mi-8 airframe, the Mi-17 was fitted with the larger TV3-117MT engines, rotors, and transmission developed for the Mi-14, along with fuselage improvements for heavier loads. Optional engines for 'hot and high' conditions are the 1545kW (2070 shp) Isotov TV3-117VM. Recent exports to China and Venezuela for use in high mountains have the new VK-2500 version of the engine with FADEC control.

The designation Mi-17 is for export; Russian armed forces call it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor on the port side instead of the starboard side, and dust shields in front of the engine intakes. Engine cowls are shorter than on the TV2 powered Mi-8, not extending as far over the cockpit, and an opening for bleed-valve outlet is present forward of the exhaust.

Actual model numbers vary by builder, engine type, and other options. As an example, the sixteen new Ulan Ude built machines delivered to the Czech Air Force in 2005 with –VM model engines were designated as Mi-171Sh, a development of the Mi-8AMTSh. Modifications include a new large door on the right side, improved Czech-built APU, Kevlar armor plates around the cockpit area and engines. Eight have a loading ramp in place of the usual clamshell doors, and will load a vehicle up to the size of an SUV.

The Mi-17 is also used for search and rescue team like Malaysian Fire and Rescue Department in Malaysia.

In October 2007 defense-aerospace.com reported the government of Saudi Arabia had signed a contract for up to 150 Mi-35 and Mi-17 helicopters worth $2.2billion.[2]

A licensed production of the Mi-17 will start in China with production being led by Mil Moscow Helicopter Plant JSC and the Sichuan Lantian Helicopter Company Limited in Chengdu, Sichuan province[3].

[edit] Operational History

The Mi-17 was used by Colombian Army in the Operation Jaque.

[edit] Variants

Mi-17V-5
Mi-17V-5
Two Egyptian Mi-17 helicopters after unloading troops during an exercise.
Two Egyptian Mi-17 helicopters after unloading troops during an exercise.
Mi-171Sh
Mi-171Sh
Malaysian Fire and Rescue Department Mi-17-1V
Malaysian Fire and Rescue Department Mi-17-1V
Mi-8AMT
Unarmed civilian transport version of the Mi-17 hip-H.
Mi-8AMT(Sh)
This version of the Mi-8AMT is built in Ulan-Ude rather than Kazan.
Mi-8MT
Uprated version of the Mi-8T, powered by two 3846-shp (2868-kW) Klimov TV3-117MT turboshaft engines. Russian designation of the Mi-17 hip-H.
Mi-8MTV
Hot and High version, fitted with a pressurised cabin, powered by two Klimov TV3-117VM turboshaft engines.
Mi-8MTV-1
Radar-equipped civil version of the Mi-8MTV. Russian designation of the Mi-17-1V.
Mi-8MTV-2
Military version of the Mi-8MTV, fitted with a radar, six weapons pylons for carrying rocket pods, missiles and other weapons.
Mi-8MTV-3
Military version of the Mi-8MTV-2, fitted with four weapons pylons.
Mi-8MTV-5
Military utility transport helicopter. Export designation Mi-17MD.
Mi-8MTV-5-Ga
Civilian version of the Mi-8MTV-5.
Mi-8MTO
Night attack conversions of the Mi-8MT and Mi-MTV helicopters.
Mi-8MTPB (NATO - Hip-H EW)
Electronic jamming version of the Mi-17 Hip-H. Export designation Mi-17PP.
Mi-8AMTSh (for export - Mi-171Sh)
Variant with new large door on the right side, kevlar plates around the cockpit area and engines. Some of them (but not all) have a loading ramp in place of the usual clamshell doors, and will load a vehicle up to the size of an SUV. Czech Republic and Croatia have ordered these types in 2005 and 2007.
Mi-17 (NATO - Hip-H)
Improved version of the Mi-8, powered by two Klimov TV3-117MT turboshaft engines. Basic production version.
Mi-17-1M
High altitude operations version, powered by two Klimov TV3-117VM turboshaft engines.
Mi-17-IV
Military transport, helicopter gunship version, powered by two Klimov TV3-117VM turboshaft engines. Also known as the Mi-8MTV-1.
Mi-17-IVA
Flying hospital version.
Mi-17MD
Export version of the Mi-8MTV-5, powered by two Klimov TV3-117VM turboshaft engines.
Mi-17KF
Export version fitted with new avionics.
Mi-17P
Export version, passenger transport helicopter.
Mi-17PG
Electronic jamming helicopter, which has a single H/I-band jamming system.
Mi-17PI
Electronic jamming helicopter, which has a single D-band jamming system.
Mi-17PP
Elecrontic jamming version of the Mi-17 Hip-H. Russian designation Mi-8MTPB.
Mi-17AE
Little-known SAR and medevac version given to Poland.
Mi-17Z-2
Czech electronic warfare version.
Mi-18
Original designation of the Mil Mi-17.
Mi-19
Airborne command post version for tank and motorized infantry commanders (based on Mi-8MT/Mi-17 airframe).
Mi-19R
Airborne command post version similar to Mi-19 for commanders of rocket artillery (based on Mi-8MT/Mi-17 airframe).
Mi-171
Fitted with more powerful turboshaft engines.
Mi-172
Civil Passenger version manufactured in Kazan plant

[edit] Operators

 Afghanistan
 Algeria
 Angola
 Armenia
 Azerbaijan
 Bangladesh
 Belarus
 Bosnia and Herzegovina
 Bulgaria
 Burkina Faso
 Cambodia
 Canada
 China
 Colombia
 Croatia 10 in service
 Cuba
 Czech Republic
 Ecuador
 Egypt
 Eritrea
 Ethiopia
 Georgia
 Hungary
 India
 Indonesia
 Iraq
 Iran
 Kazakhstan
 Kenya
 Kyrgyzstan
 Laos
 Latvia
 Lithuania
 Republic of Macedonia
 Malaysia
(Fire and Rescue version)[1]
 Mexico

Mongolia

 Myanmar
 Nepal
 Nicaragua
 North Korea
 Pakistan
 Papua New Guinea
 Peru
 Poland
 Romania
 Russia
 Rwanda
(Mi-17MD)
 Saudi Arabia
 Serbia
 Sierra Leone
 Slovakia
 Sri Lanka
 Syria
 Tajikistan
 Turkey
18 in service with Police Service
 Turkmenistan
 Uganda
 Ukraine
 Uzbekistan
 Venezuela
 Vietnam

[edit] Incidents

[edit] Specifications (Mil-17)

General characteristics

  • Crew: Three – two pilots and one engineer
  • Capacity: 32 passengers or 4,000 kg (8,800 lb) on internal/4,500 kg (10,250 lb) external hardpoints.
  • Length: 18.42 m (60 ft 5 in)
  • Rotor diameter: 21.352 m (69 ft 10 in)
  • Height: 4.76 m (15 ft 7 in)
  • Disc area: 356 m² (3,830 ft²)
  • Empty weight: 7,100 kg (15,700 lb)
  • Loaded weight: 11,100 kg (24,470 lb)
  • Max takeoff weight: 13,000 kg (28,700 lb)
  • Powerplant:Klimov TV3-117VM turboshafts, 1,450 kW (2225 shp) each

Performance

  • Fuel consumption: 600 kg/h (1,320 lb/h)

Armament

  • up to 1,500 kg (3,300 lb) of disposable stores on six hardpoints, including bombs, rockets, and gunpods.

[edit] See also

Wikimedia Commons has media related to:

Related development

Comparable aircraft

[edit] References

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

[edit] External links

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