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Mi-17 Hip-H

Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions.

Mil Mi-17 Hip-H military helicopters in flight
Origin country
๐Ÿ‡ท๐Ÿ‡บ Ex-USSR
First flight
1975Jan 1
Introduced
1977
Produced
12,000units
Avg unit price
$15 million
Active worldwide
804
Mil Mi-17 Hip-H military helicopters side profile drawing
Side profile ยท Mil Mi-17 Hip-H ยท length 18.5 m
Technical SpecificationsVersion: Mi-17-1V
Crew3 members
Length18.5 m (60.6 ft)
Wingspan21.3 m (69.7 ft)
Height4.8 m (15.6 ft)
Empty weight7,489 kg (16,510 lbs)
Max. takeoff weight13,000 kg (28,660 lbs)
Powerplant2 ร— turboprops Klimov TV3-117VM 746 kW each
PerformanceVersion: Mi-17-1V
Maximum speed250 km/h (155 mph)
Operational range800 km (497 mi)
Service ceiling6,000 m (19,685 ft)
Climb rate8.0 m/s (26.2 ft/s)
Operators โ€” 2026
ActiveOn order
Live Losses TrackerUpdated daily

4 losses recorded here in the 2026 Iran Conflict.

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Mi-17 Hip-H vs
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๐Ÿ‡ง๐Ÿ‡ฉ Bangladeshยท ๐Ÿ‡ง๐Ÿ‡ฌ Bulgariaยท ๐Ÿ‡จ๐Ÿ‡ณ Chinaยท ๐Ÿ‡จ๐Ÿ‡ฒ Cameroonยท ๐Ÿ‡จ๐Ÿ‡ด Colombiaยท ๐Ÿ‡จ๐Ÿ‡ป Cape Verdeยท ๐Ÿ‡จ๐Ÿ‡ท Costa Ricaยท ๐Ÿ‡จ๐Ÿ‡บ Cubaยท ๐Ÿ‡จ๐Ÿ‡ฟ Czechiaยท ๐Ÿ‡ช๐Ÿ‡จ Ecuadorยท ๐Ÿ‡ช๐Ÿ‡ท Eritreaยท ๐Ÿ‡ฌ๐Ÿ‡ญ Ghanaยท ๐Ÿ‡ฌ๐Ÿ‡ณ Guineaยท ๐Ÿ‡ฌ๐Ÿ‡ถ Equatorial Guineaยท ๐Ÿ‡ญ๐Ÿ‡ท Croatiaยท ๐Ÿ‡ฎ๐Ÿ‡ฉ Indonesiaยท ๐Ÿ‡ฎ๐Ÿ‡ณ Indiaยท ๐Ÿ‡ฎ๐Ÿ‡ท Iranยท ๐Ÿ‡ฐ๐Ÿ‡ฟ Kazakhstanยท ๐Ÿ‡ฐ๐Ÿ‡ช Kenyaยท ๐Ÿ‡ฑ๐Ÿ‡ฆ Laosยท ๐Ÿ‡ฑ๐Ÿ‡ท Liberiaยท ๐Ÿ‡ฑ๐Ÿ‡พ Libyaยท ๐Ÿ‡ฒ๐Ÿ‡ฝ Mexicoยท ๐Ÿ‡ฒ๐Ÿ‡ฒ Myanmarยท ๐Ÿ‡ฒ๐Ÿ‡ณ Mongoliaยท ๐Ÿ‡ณ๐Ÿ‡ช Nigerยท ๐Ÿ‡ณ๐Ÿ‡ฌ Nigeriaยท ๐Ÿ‡ณ๐Ÿ‡ต Nepalยท ๐Ÿ‡ต๐Ÿ‡ช Peruยท ๐Ÿ‡ต๐Ÿ‡ฌ Papua New Guineaยท ๐Ÿ‡ท๐Ÿ‡ผ Rwandaยท ๐Ÿ‡ธ๐Ÿ‡ณ Senegalยท ๐Ÿ‡ธ๐Ÿ‡ฑ Sierra Leoneยท ๐Ÿ‡ธ๐Ÿ‡ธ South Sudanยท ๐Ÿ‡ธ๐Ÿ‡ฐ Slovakiaยท ๐Ÿ‡น๐Ÿ‡ฒ Turkmenistanยท ๐Ÿ‡บ๐Ÿ‡ฌ Ugandaยท ๐Ÿ‡บ๐Ÿ‡ธ United Statesยท ๐Ÿ‡ป๐Ÿ‡ช Venezuelaยท ๐Ÿ‡ฟ๐Ÿ‡ฒ Zambiaยท ๐Ÿ‡ฟ๐Ÿ‡ผ Zimbabwe

Description

Developed from the basic Mi-8 airframe, the Mi-17 incorporates larger Klimov TV3-117MT engines, along with enhanced rotors and transmission derived from the Mi-14, enabling greater load capacities through fuselage improvements. Optional 1,545 kW (2,072 shp) Isotov TV3-117VM engines are available for operations in hot and high conditions. More recent export models feature the Klimov VK-2500 engine, a version of the Klimov TV3-117 with FADEC control optimized for high-altitude performance, delivered to regions including China and Venezuela for high mountain operations. Officially, the designation Mi-17 is for export; the Russian armed forces refer to it as the Mi-8MT. Distinguishing features of the Mi-17 include a tail rotor positioned on the port side (as opposed to the starboard side on the Mi-8), the inclusion of dust shields in front of the engine intakes, and shorter engine cowls than those on the TV2-powered Mi-8, which do not extend as far over the cockpit and feature an opening for a bleed air valve outlet forward of the exhaust. The Mil Mi-17 family was introduced in 1975 with the Mi-8M, and continues in production as of 2024. Modifications may include a new large door on the right side, an improved APU built in the Czechia, and Kevlar armour around the cockpit area and engines, with some models featuring a loading ramp in place of the standard clamshell doors.

Armament

Some variants of the Mi-17, particularly the Mi-8AMTSh and Mi-171Sh, feature six hardpoints for mounting disposable stores, enabling them to carry a diverse range of weaponry. These can include unguided rockets, such as the S-8, and gun pods like the UPK-23-250. Advanced versions, such as the Mi-171SH-HV and Mi-171SH-VN, expand their offensive capabilities with anti-tank guided missiles, such as the Ataka, and precision-guided munitions. Defensive armament typically includes one or two window-mounted PK machine guns. Additionally, the hardpoints can accommodate drop tanks to extend the helicopter's operational range or carry up to 4,000 kg (8,800 lb) of bombs.

Operational History

The Royal Cambodian Air Force deployed its Mi-17s during government offensives, with ten airframes operational by 1994, five of which were converted into helicopter gunships armed with 57 mm S-5 rocket pods to support ground forces against Khmer Rouge positions. Similarly, in 1999, the Indian Air Force utilized Mi-17s during the Kargil War, though the loss of one Mi-17 and an escorting MiG-21 to Pakistani air defenses led to a shift towards fixed-wing aircraft for attacks. The Sri Lanka Air Force also relied heavily on the Mi-17 in its conflict against the LTTE, incurring the loss of seven helicopters in combat and airport attacks. In other theaters, freelance pilots like Neall Ellis operated Mi-17s to support the Sierra Leone government during the Sierra Leone Civil War. US Army Special Forces in Afghanistan also used CIA-operated Mi-17s during the initial stages of Operation Enduring Freedom, demonstrating the helicopter's versatility and widespread utility across diverse operational environments.

Variants

Main Variants:

  • Mi-8MT: The basic updated version of the Mi-8T, distinguished by its more powerful Klimov TV3-117MT turboshaft engines and the provision for external stores racks.

  • Mi-8MTV: A hot and high conditions variant, featuring Klimov TV3-117VM high-altitude turboshaft engines, enabling operations at a maximum ceiling of 6,000 m.

  • Mi-8MTV-5: A military utility transport helicopter equipped with a loading ramp, an additional door, a new "dolphin nose," and Klimov TV3-117VM turboshaft engines.

  • Mi-8AMT: A slightly modified version of Kazan's Mi-8MTV, built in Ulan-Ude Aviation Plant, initially powered by TV3-117VM engines and later optionally by VK-2500 engines, with an arctic version entering production in 2020.

  • Mi-8AMTSh: An armed assault version of the Mi-8AMT capable of carrying a wide range of weapons, enhanced with aramid fiber plates, and featuring a new large door, as well as an optional loading ramp.

Frequently Asked Questions

What type of aircraft is the Mi-17 Hip-H?
The Mil Mi-17 Hip-H is a military helicopters aircraft developed by Mil and entered service in 1977.
What is the maximum speed of the Mi-17 Hip-H?
The Mil Mi-17 Hip-H has a maximum speed of 250 km/h (155 mph).
What is the range of the Mi-17 Hip-H?
The Mil Mi-17 Hip-H has an operational range of 800 km (497 miles). This range can vary based on payload, altitude, and mission profile.
When did the Mi-17 Hip-H first fly?
The Mil Mi-17 Hip-H made its first flight on January 01, 1975. It entered operational service in 1977.
How many Mi-17 Hip-H have been built?
Approximately 12,000 units of the Mil Mi-17 Hip-H have been produced since it entered service in 1977.
Which countries operate the Mi-17 Hip-H?
The Mil Mi-17 Hip-H is operated by 36 countries with approximately 804 aircraft in active service. The largest operators include China, India, and Bangladesh.
How much does a Mi-17 Hip-H cost?
The Mil Mi-17 Hip-H has an estimated unit cost of approximately $15.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Mi-17 Hip-H?
The Mil Mi-17 Hip-H has a service ceiling of 6,000 meters (19,685 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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