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Mi-8 Hip

Soviet multipurpose helicopter, prevalent during the Cold War, extensively utilized for transport, combat and humanitarian operations globally. Key figures: top speed 250 km/h, range 495 km, service ceiling 4,500 m, max takeoff weight 12,000 kg, unit price $4M, built 17,000. In service with 51 air forces as of 2026 — Russia (789), Algeria (140), Ukraine (73) and 48 others.

Mil Mi-8 Hip military helicopters side profile drawing
Side profile · Mil Mi-8 Hip · length 25.2 m
Mil Mi-8 Hip military helicopters in flight
Max speed
250km/h
Range
495km
Produced
17,000units
Avg unit price
$4 million
Active worldwide
1,896+12 on order
Technical SpecificationsVersion: Mi-8T Hip-C
Crew3 (2 pilots, flight engineer)
Length25.2 m (82.8 ft)
Wingspan21.3 m (69.8 ft)
Height5.7 m (18.5 ft)
Empty weight7,160 kg (15,785 lbs)
Max. takeoff weight12,000 kg (26,455 lbs)
Powerplant2 × turboshafts Klimov TV2-117 1,119 kW each
PerformanceVersion: Mi-8T Hip-C
Maximum speed250 km/h (155 mph)
Operational range495 km (308 mi)
Service ceiling4,500 m (14,764 ft)
All Operators
🇦🇫 Afghanistan· 🇦🇴 Angola· 🇦🇲 Armenia· 🇦🇿 Azerbaijan· 🇧🇫 Burkina Faso· 🇧🇩 Bangladesh· 🇧🇬 Bulgaria· 🇧🇦 Bosnia and Herzegovina· 🇧🇾 Belarus· 🇧🇴 Bolivia· 🇧🇹 Bhutan· 🇨🇫 Central African Republic· 🇨🇳 China· 🇨🇮 Ivory Coast· 🇨🇩 Congo Democratic Republic· 🇨🇬 Congo· 🇨🇴 Colombia· 🇨🇷 Costa Rica· 🇨🇺 Cuba· 🇨🇿 Czechia· 🇩🇪 Germany· 🇩🇯 Djibouti· 🇩🇿 Algeria· 🇪🇬 Egypt· 🇪🇪 Estonia· 🇪🇹 Ethiopia· 🇫🇮 Finland· 🇬🇪 Georgia· 🇬🇾 Guyana· 🇭🇷 Croatia· 🇭🇺 Hungary· 🇮🇩 Indonesia· 🇮🇳 India· 🇮🇷 Iran· 🇮🇶 Iraq· 🇰🇿 Kazakhstan· 🇰🇬 Kyrgyzstan· 🇰🇭 Cambodia· 🇱🇾 Libya· 🇱🇰 Sri Lanka· 🇱🇹 Lithuania· 🇱🇻 Latvia· 🇲🇩 Moldova· 🇲🇬 Madagascar· 🇲🇽 Mexico· 🇲🇰 North Macedonia· 🇲🇱 Mali· 🇲🇲 Myanmar· 🇲🇳 Mongolia· 🇲🇿 Mozambique· 🇲🇾 Malaysia· 🇳🇦 Namibia· 🇳🇮 Nicaragua· 🇵🇰 Pakistan· 🇵🇪 Peru· 🇵🇱 Poland· 🇰🇵 North Korea· 🇷🇺 Russia· 🇸🇩 Sudan· 🇷🇸 Serbia· 🇸🇰 Slovakia· 🇸🇾 Syria· 🇹🇩 Chad· 🇹🇬 Togo· 🇹🇭 Thailand· 🇹🇯 Tajikistan· 🇹🇲 Turkmenistan· 🇹🇷 Turkey· 🇺🇦 Ukraine· 🇺🇸 United States· 🇺🇿 Uzbekistan· 🇻🇳 Vietnam· 🇾🇪 Yemen· 🇷🇸 Ex-Yugoslavia· 🇿🇲 Zambia
Air Bases — 18
🇧🇾 Luninets Air Base 1169th Aviation Equipment Reserve Base 🇮🇳 Car Nicobar AFS No. 122 Helicopter Flight 🇮🇳 Kumbhigram AFS No. 110 Helicopter Unit 🇲🇽 Campeche Naval Air Base 5th Air Mobility, Observation and Transport Naval Air Squadron 🇷🇺 Chelyabinsk Air Base 108th Training Aviation Regiment 🇷🇺 Dolinsk-Sokol Air Base 361st Instruction Test Helicopter Regiment 🇷🇺 Kapustin Yar Air Base 35th independent mixed air squadron 🇷🇺 Kubinka Air Base 378th Independent Composite Aviation Squadron 🇷🇺 Levashovo Air Base 549th Air Base 🇷🇺 Monchegorsk Air Base 7000 air group aerodrome 🇷🇺 Pushkin-3 Air Base 147 OVZ RZB regiment 🇷🇺 Tiksi Air Base 200th Guards Heavy Bomber Aviation Regiment 🇸🇾 Menagh Air Base 4 Squadron 🇸🇾 Taftanaz Air Base 253 Squadron 🇺🇦 Brody Air Base 16th Separate Army Aviation Brigade 🇺🇦 Kacha Air Base 25th Independent Shipborne Anti-submarine Helicopter Regiment 🇺🇿 Chirchik Air Base 66th Separate Helicopter Regiment 🇻🇳 Vũng Tàu Airfield Southern Service Flight Company
Similar Aircraft
Mi-8 Hip vs

Description

The Mil Mi-8 (NATO reporting name: Hip) is a Soviet-designed medium twin-turbine helicopter originally developed by the Mil Design Bureau and produced by the Kazan Production Plant. Introduced into the Soviet Air Force in 1967, the aircraft operates as a transport, airborne command post, armed gunship, and reconnaissance platform. With over 17,000 units built and used by more than 50 countries, the Mi-8 is the most-produced helicopter in history.

Development

Mikhail Mil proposed a twin-engine turbine replacement for the Mil Mi-4 in 1959. The single-engine V-8 prototype made its maiden flight in June 1961, followed on 2 August 1962 by the V-8A prototype equipped with two Isotov TV2 turboshaft engines, marking the first Soviet helicopter flown with purpose-built gas turbines. Government testing concluded in November 1964, leading to mass production at the Kazan plant in late 1965.

Design

The Mi-8 features a five-blade main rotor introduced in 1963 to reduce vibration and a main cabin designed to accommodate up to 24 passengers or 4,000 kg of cargo. Second-generation models transitioned from a right-side pusher tail rotor to a left-side tractor configuration to increase yaw authority across advancing rotor blades. Power on the Mi-8MT variant is supplied by twin Klimov TV3-117MT turboshaft engines producing 1,454 kW each.

Armament

Armed variants carry up to 4,000 kg of stores across four to six external hardpoints. Munitions include 57 mm S-5 unguided rockets in UV-16-57 or UV-32-57 pods, 250 kg bombs, and anti-tank guided missiles such as the AT-2 Swatter, 9M17 Phalanga, or Malyutka. Defensive machine guns include side-mounted 7.62 mm PK guns or a nose-mounted flexible 12.7 mm KV-4 machine gun.

Operational History

The Soviet Union deployed fleets of Mi-8s during the Soviet–Afghan War and used them to drop over 5,000 metric tons of materials onto the Chernobyl reactor in 1986. The type saw combat during the Iran–Iraq War, the War in Abkhazia, the Yugoslav Wars, and the Russo-Ukrainian War. Export customers and operators include Finland, Georgia, India, Iraq, Ukraine, and Yugoslavia.

Variants

  • Mi-8T: First mass-production utility transport variant capable of carrying 24 troops, unguided rocket pods, and side-mounted machine guns.

  • Mi-8TVK: Direct air support gunship variant fitted with six external hardpoints and a flexible 12.7 mm nose machine gun.

  • Mi-8IV: Airborne command post variant equipped with the Ivolga communication system and tail-boom Doppler radar.

  • Mi-8PP: Airborne electronic warfare platform fitted with the Polye jamming system to disrupt ground-based air defense radars.

  • Mi-8P: Civilian passenger transport variant powered by twin Klimov TV2-117A engines with seating for up to 32 passengers.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 6 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Mi-8 Hip?
The Mil Mi-8 Hip is a military helicopters aircraft developed by Mil and entered service in 1967.
What is the maximum speed of the Mi-8 Hip?
The Mil Mi-8 Hip has a maximum speed of 250 km/h (155 mph).
What is the range of the Mi-8 Hip?
The Mil Mi-8 Hip has an operational range of 495 km (307 miles). This range can vary based on payload, altitude, and mission profile.
When did the Mi-8 Hip first fly?
The Mil Mi-8 Hip made its first flight on June 24, 1961. It entered operational service in 1967.
How many Mi-8 Hip have been built?
Approximately 17,000 units of the Mil Mi-8 Hip have been produced since it entered service in 1967.
Which countries operate the Mi-8 Hip?
The Mil Mi-8 Hip is operated by 51 countries with approximately 1,896 aircraft in active service. The largest operators include Russia, Algeria, and Ukraine.
How much does a Mi-8 Hip cost?
The Mil Mi-8 Hip has an estimated unit cost of approximately $4.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Mi-8 Hip?
The Mil Mi-8 Hip has a service ceiling of 4,500 meters (14,763 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Latest Data Updates
  1. AUG 62026 Updated Description updated
  2. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  3. JUL 232026 Updated Sources and cross-references refreshed
  4. APR 72026 Updated Sources and cross-references refreshed
  5. JAN 122026 Updated Range updated in a site-wide editorial pass