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Mil Mi-24
Mil Mi-24
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The Mil Mi-24 (Russian: Миль Ми-24; NATO reporting name: Hind) is a large helicopter gunship, attack helicopter and low-capacity troop transport with room for eight passengers.[1] It is produced by Mil Moscow Helicopter Plant and was introduced by the Soviet Air Force in 1972. The helicopter is[when?] in use with 58 countries.

Key Information

In NATO circles, the export versions, Mi-25 and Mi-35, are denoted with a letter suffix as "Hind D" and "Hind E". Soviet pilots called the Mi-24 the "flying tank" (Russian: летающий танк, romanized: letayushchiy tank), a term used historically with the famous World War II Soviet Il-2 Shturmovik armored ground attack aircraft. Other common unofficial nicknames were "Galina" (or "Galya"), "Crocodile" (Russian: Крокодил, romanized: Krokodil), due to the helicopter's camouflage scheme, and "Drinking Glass" (Russian: Стакан, romanized: Stakan), because of the flat glass plates that surround earlier Mi-24 variants' cockpits.[2]

Development

[edit]

During the early 1960s, it became apparent to Soviet designer Mikhail Mil that the trend towards ever-increasing battlefield mobility would result in the creation of flying infantry fighting vehicles, which could be used to perform both fire support and infantry transport missions. The first expression of this concept was a mock-up unveiled in 1966 in the experimental department of the Ministry of Aircraft's factory number 329, where Mil was head designer. The mock-up designated V-24 was based on another project, the V-22 utility helicopter, which never flew. The V-24 had a central infantry compartment that could hold eight troops sitting back to back, and a set of small wings positioned to the top rear of the passenger cabin, capable of holding up to six missiles or rockets and a twin-barreled GSh-23L cannon fixed to the landing skid.

Mil Mi-24A, Riga airport aviation museum

Mil proposed the design to the heads of the Soviet armed forces. While he had the support of a number of strategists, he was opposed by several more senior members of the armed forces, who believed that conventional weapons were a better use of resources. Despite the opposition, Mil managed to persuade the defence minister's first deputy, Marshal Andrey A. Grechko, to convene an expert panel to look into the matter. While the panel's opinions were mixed, supporters of the project eventually held sway and a request for design proposals for a battlefield support helicopter was issued. The development and use of gunships and attack helicopters by the US Army during the Vietnam War convinced the Soviets of the advantages of armed helicopter ground support, and fostered support for the development of the Mi-24.[3]

Mil engineers prepared two basic designs: a 7-ton single-engine design and a 10.5-ton twin-engine design, both based on the 1,700 hp Izotov TV3-177A turboshaft. Later, three complete mock-ups were produced, along with five cockpit mock-ups to allow the pilot and weapon station operator positions to be fine-tuned.

The Kamov design bureau suggested an army version of their Ka-25 ASW helicopter as a low-cost option. This was considered but later dropped in favor of the new Mil twin-engine design. A number of changes were made at the insistence of the military, including the replacement of the 23 mm cannon with a rapid-fire heavy machine gun mounted in a chin turret, and the use of the 9K114 Shturm (AT-6 Spiral) anti-tank missile.

A directive was issued on 6 May 1968 to proceed with the development of the twin-engine design. Work proceeded under Mil until his death in 1970. Detailed design work began in August 1968 under the codename Yellow 24. A full-scale mock-up of the design was reviewed and approved in February 1969. Flight tests with a prototype began on 15 September 1969 with a tethered hover, and four days later the first free flight was conducted. A second prototype was built, followed by a test batch of ten helicopters.

Russian Air Force Mil Mi-24P

Acceptance testing for the design began in June 1970, continuing for 18 months. Changes made in the design addressed structural strength, fatigue problems and vibration levels. Also, a 12-degree anhedral was introduced to the wings to address the aircraft's tendency to Dutch roll at speeds in excess of 200 km/h (124 mph), and the Falanga missile pylons were moved from the fuselage to the wingtips. The tail rotor was moved from the right to the left side of the tail, and the rotation direction reversed. The tail rotor now rotated up on the side towards the front of the aircraft, into the downwash of the rotor, which increased its efficiency. A number of other design changes were made until the production version Mi-24A (izdeliye 245) entered production in 1970, obtaining its initial operating capability in 1971 and was officially accepted into the state arsenal in 1972.[4]

In 1972, following completion of the Mi-24, development began on a unique attack helicopter with transport capability. The new design had a reduced transport capability (three troops instead of eight) and was called the Mi-28, and that of the Ka-50 attack helicopter, which is smaller and more maneuverable and does not have the large cabin for carrying troops. In October 2007, the Russian Air Force announced it would replace its Mi-24 fleet with Mi-28Ns and Ka-52s by 2015.[5][6] However, after the successful operation of the type in Syria it was decided to keep it in service and upgrade it with new electronics, sights, arms and night vision goggles.[7]

Design

[edit]

Overview

[edit]
Russian Air Force Mi-35М

The core of the aircraft was derived from the Mil Mi-8 (NATO reporting name "Hip") with two top-mounted turboshaft engines driving a mid-mounted 17.3 m (57 ft) five-blade main rotor and a three-blade tail rotor. The engine configuration gave the aircraft its distinctive double air intake. Original versions have an angular greenhouse-style cockpit; Model D and later have a characteristic tandem cockpit with a "double bubble" canopy. Other airframe components came from the Mi-14 "Haze". Two mid-mounted stub wings provide weapon hardpoints, each offering three stations, in addition to providing lift. The loadout mix is mission dependent; Mi-24s can be tasked with close air support, anti-tank operations, or aerial combat.

The Mi-24's titanium rotor blades are resistant to 12.7 mm (.50 caliber) rounds.[citation needed] The cockpit is protected by ballistic-resistant windscreens and a titanium-armored tub.[8] The cockpit and crew compartment are overpressurized to protect the crew in NBC conditions.[9]

Flight characteristics

[edit]
Mi-24D cockpit
Mi-35M with the OPS-24N survey and sighting system together with the gyrostabilized OLS GOES-324

Considerable attention was given to making the Mi-24 fast. The airframe was streamlined, and fitted with retractable tricycle undercarriage landing gear to reduce drag. At high speed, the wings provide considerable lift (up to a quarter of total lift). The main rotor was tilted 2.5° to the right from the fuselage to compensate for translating tendency at a hover. The landing gear was also tilted to the left so that the rotor would still be level when the aircraft was on the ground, making the rest of the airframe tilt to the left. The tail was also asymmetrical to give a side force at speed, thus unloading the tail rotor.[10]

A modified Mi-24B, named A-10, was used in several speed and time-to-climb world record attempts. The helicopter had been modified to reduce weight as much as possible—one measure was the removal of the stub wings.[4] The previous official speed record was set on 13 August 1975 over a closed 1,000 km (620 mi) course of 332.65 km/h (206.70 mph); many of the female-specific records were set by the all-female crew of Galina Rastorguyeva and Lyudmila Polyanskaya.[11] On 21 September 1978, the A-10 set the absolute speed record for helicopters with 368.4 km/h (228.9 mph) over a 15/25 km course. The record stood until 1986, when it was broken by the current official record holder, a modified British Westland Lynx.[12]

Comparison to Western helicopters

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U.S. operated Mi-24P Hind-F
Mi-24 SuperHind, a modernized Hind by the South African firm ATE. At the Ysterplaat Airshow 2006.

As a combination of armoured gunship and troop transport, the Mi-24 has no direct NATO counterpart. While the UH-1 ("Huey") helicopters were used by the US in the Vietnam War either to ferry troops, or as gunships, they were not able to do both at the same time. Converting a UH-1 into a gunship meant stripping the entire passenger area to accommodate extra fuel and ammunition, and removing its troop transport capability. The Mi-24 was designed to do both, and this was greatly exploited by airborne units of the Soviet Army during the 1980–89 Soviet–Afghan War. The closest Western equivalent was the American Sikorsky S-67 Blackhawk, which used many of the same design principles and was also built as a high-speed, high-agility attack helicopter with limited troop transport capability using many components from the existing Sikorsky S-61. The S-67, however, was never adopted for service.[1] Other Western equivalents are the Romanian Army's IAR 330, which is a licence-built armed version of the Aérospatiale SA 330 Puma, and the MH-60 Direct Action Penetrator, a special purpose armed variant of the Sikorsky UH-60 Black Hawk.

Operational history

[edit]

Ogaden War (1977–1978)

[edit]

The first combat use of the Mi-24 was with the Ethiopian forces during the Ogaden War against Somalia. The helicopters formed part of a massive airlift of military equipment from the Soviet Union, after the Soviets switched sides towards the end of 1977. The helicopters were instrumental in the combined air and ground assault that allowed the Ethiopians to retake the Ogaden by the beginning of 1978.[13]

Chadian–Libyan conflict (1978–1987)

[edit]

The Libyan air force used Mi-24A and Mi-25 units during their numerous interventions in Chad's civil war.[10] The Mi-24s were first used in October 1980 in the battle of N'Djamena, where they helped the People's Armed Forces seize the capital.

In March 1987, the Armed Forces of the North, which were backed by the US and France, captured a Libyan air force base at Ouadi-Doum in Northern Chad. Among the aircraft captured during this raid were three Mi-25s. These were supplied to France, which in turn sent one to the United Kingdom and one to the US.[4]

Soviet war in Afghanistan (1979–1989)

[edit]
Front view of a Soviet Mi-24 HIND E ground-attack helicopter

The aircraft was operated extensively during the Soviet–Afghan War, mainly for bombing Mujahideen fighters. When the U.S. supplied heat-seeking Stinger missiles to the Mujahideen, the Soviet Mi-8 and Mi-24 helicopters proved to be favorite targets of the rebels.

It is difficult to find the total number of Mi-24s used in Afghanistan.[14] At the end of 1990, the whole Soviet Army had 1,420 Mi-24s.[15] During the Afghan war, sources estimated the helicopter strength to be as much as 600 units, with up to 250 being Mi-24s,[16] whereas a (formerly secret) 1987 Central Intelligence Agency (CIA) report says that the number of Mi-24s in theatre increased from 85 in 1980 to 120 in 1985.[17]

First deployment and combat

[edit]

In April 1979, Mi-24s were supplied to the Afghan government to deal with Mujahideen guerrillas.[18] The Afghan pilots were well-trained and made effective use of their machines, but the Mujahideen were not easy targets. The first Mi-24 to be lost in action was shot down by guerrillas on 18 July 1979.[19][20]

Soviet "Helicopter-tank" operation in Afghanistan

Despite facing strong resistance from Afghan rebels, the Mi-24 proved to be very destructive. The rebels called the Mi-24 "Shaitan-Arba (Satan's Chariot)".[18] In one case, an Mi-24 pilot who was out of ammunition managed to rescue a company of infantry by maneuvering aggressively towards Mujahideen guerrillas and scaring them off. The Mi-24 was popular with ground troops, since it could stay on the battlefield and provide fire as needed, while "fast mover" strike jets could only stay for a short time before heading back to base to refuel.

The Mi-24's favoured munition was the 80-millimetre (3.1 in) S-8 rocket, the 57 mm (2.2 in) S-5 having proven too light to be effective. The 23 mm (0.91 in) gun pod was also popular. Extra rounds of rocket ammunition were often carried internally so that the crew could land and self-reload in the field. The Mi-24 could carry ten 100-kilogram (220 lb) iron bombs for attacks on camps or strongpoints, while harder targets could be dealt with a load of four 250-kilogram (550 lb) or two 500-kilogram (1,100 lb) iron bombs.[21] Some Mi-24 crews became experts at dropping bombs precisely on targets. Fuel-air explosive bombs were also used in a few instances, though crews initially underestimated the sheer blast force of such weapons and were caught by the shock waves. The 9K114 Shturm was used infrequently, largely due to a lack of targets early in the war that required the precision and range the missile offered and a need to keep to stocks of anti tank missiles in Europe. After the Mujahideen got access to more advanced anti aircraft weapons later in the war the Shturm was used more often by Mi-24 units.[22]

Combat experience quickly demonstrated the disadvantages of having an Mi-24 carrying troops. Gunship crews found the soldiers a concern and a distraction while being shot at, and preferred to fly lightly loaded anyway, especially given their operations from high ground altitudes in Afghanistan. Mi-24 troop compartment armour was often removed to reduce weight. Troops would be carried in Mi-8 helicopters while the Mi-24s provided fire support.

Mil Mi-24/25

It proved useful to carry a technician in the Mi-24's crew compartment to handle a light machine gun in a window port. This gave the Mi-24 some ability to "watch its back" while leaving a target area. In some cases, a light machine gun was fitted on both sides to allow the technician to move from one side to the other without having to take the machine gun with him.

This weapon configuration still left the gunship blind to the direct rear, and Mil experimented with fitting a machine gun in the back of the fuselage, accessible to the gunner through a narrow crawl-way. The experiment was highly unsuccessful, as the space was cramped, full of engine exhaust fumes, and otherwise unbearable. During a demonstration, an overweight Soviet Air Force general got stuck in the crawl-way.[4] Operational Mi-24s were retrofitted with rear-view mirrors to help the pilot spot threats and take evasive action.

Besides protecting helicopter troop assaults and supporting ground actions, the Mi-24 also protected convoys, using rockets with flechette warheads to drive off ambushes; performed strikes on predesignated targets; and engaged in "hunter-killer" sweeps. Hunter-killer Mi-24s operated at a minimum in pairs, but were more often in groups of four or eight, to provide mutual fire support. The Mujahideen learned to move mostly at night to avoid the gunships, and in response the Soviets trained their Mi-24 crews in night-fighting, dropping parachute flares to illuminate potential targets for attack. The Mujahideen quickly caught on and scattered as quickly as possible when Soviet target designation flares were lit nearby.

Attrition in Afghanistan

[edit]

The war in Afghanistan brought with it losses by attrition.[18] The environment itself, dusty and often hot, was rough on the machines; dusty conditions led to the development of the twin PZU ('PyleZashchitnoe Ustroystvo') air intake filters. The rebels' primary air-defence weapons early in the war were heavy machine guns and anti-aircraft cannons, though anything smaller than a 23 millimetre shell generally did not do much damage to an Mi-24. The cockpit glass panels were resistant to 12.7 mm (.50 in calibre) rounds.[citation needed]

The rebels also quickly began to use Soviet-made and US shoulder-launched, man-portable air-defense system (MANPADS) missiles such as the Strela and Redeye which had either been captured from the Soviets or their Afghan allies or were supplied from Western sources. Many of them came from stocks that the Israelis had captured during wars with Soviet backed states in the Middle East. Owing to a combination of the limited capabilities of these early types of missiles, poor training and poor material condition of the missiles, they were not particularly effective. Instead, the RPG-7, originally developed as an antitank weapon, was the first effective countermeasure to the Hind. The RPG-7, not designed for air defence, had inherent shortcomings in this role. When fired at the angles needed to hit aerial targets, the back-blast could easily wound the shooter, and the inevitable cloud of smoke and dust made it easy for gunners to spot the shooter's position.[citation needed]

From 1986,[21] the CIA began supplying the Afghan rebels with newer Stinger shoulder-launched, heat-seeking SAMs.[23] These were a marked improvement over earlier weapons. Unlike the Redeye and SA-7, which locked on to only infrared emissions, the Stinger could lock onto both infrared and ultraviolet emissions. This enabled the operator to engage an aircraft from all angles rather than just the tail and made it significantly more resistant to countermeasures like flares. In addition the Mil helicopters, particularly the Mi-24, suffered from a design flaw in the configuration of their engines that made them highly vulnerable to the Stinger. The Mi-24, along with the related Mi-8 and Mi-17 helicopters, had its engines placed in an inline configuration in an attempt to streamline the helicopter to increase speed and minimize the aircraft's overall frontal profile to incoming fire in a head on attack. However this had the opposite effect of leaking all the exhaust gasses from the Mi-24's engines directly out the side of the aircraft and away from the helicopter's rotor wash, creating two massive sources of heat and ultraviolet radiation for the Stinger to lock onto.[24] The inline placement of the engines was seen as so problematic in this regard that Mil designers abandoned the configuration on the planned successor to the Mi-24, the Mil Mi-28, in favour of an engine placement more akin to Western attack helicopters which vents the exhaust gasses into the helicopter's main rotor wash to dissipate heat.[citation needed]

Initially, the attack doctrine of the Mi-24 was to approach its target from high altitude and dive downwards. After the introduction of the Stinger, doctrine changed to "nap of the earth" flying, where they approached very low to the ground and engaged more laterally, popping up to only about 200 ft (61 m) in order to aim rockets or cannons.[25] Countermeasure flares and missile warning systems would be installed in all Soviet Mil Mi-2, Mi-8, and Mi-24 helicopters, giving pilots a chance to evade missiles fired at them. Heat dissipation devices were also fitted to exhausts to decrease the Mi-24's heat signature. Tactical and doctrinal changes were introduced to make it harder for the enemy to deploy these weapons effectively. These reduced the Stinger threat, but did not eliminate it.

Mi-24s were also used to shield jet transports flying in and out of Kabul from Stingers. The gunships carried flares to blind the heat-seeking missiles. The crews called themselves "Mandatory Matrosovs", after a Soviet hero of World War II who threw himself across a German machine gun to let his comrades break through.[citation needed]

According to Russian sources, 74 helicopters were lost, including 27 shot down by Stinger and two by Redeye.[21] In many cases, the helicopters with their armour and durable construction could withstand significant damage and able to return to base.[citation needed]

Mi-24 crews and end of Soviet involvement

[edit]

Mi-24 crews carried AK-74 assault rifles and other hand-held weapons to give them a better chance of survival if forced down.[18] Early in the war, Marat Tischenko, head of the Mil design bureau visited Afghanistan to see what the troops thought of his helicopters, and gunship crews put on several displays for him. They even demonstrated manoeuvres, such as barrel rolls, which design engineers considered impossible. An astounded Tischenko commented, "I thought I knew what my helicopters could do, now I'm not so sure!"[18]

The last Soviet Mi-24 shot down was during the night of 2 February 1989, with both crewmen killed. It was also the last Soviet helicopter lost during nearly 10 years of warfare.[21]

Mi-24s in Afghanistan after Soviet withdrawal

[edit]
Two Mil Mi-35 Hind helicopters during a training sortie over southern Afghanistan, 4 October 2009. U.S. Airmen with the 438th Air Expeditionary Training Group.

Mi-24s passed on to Soviet-backed Afghan forces during the war remained in dwindling service in the grinding civil war that continued after the Soviet withdrawal.[18]

Afghan Air Force Mi-24s in the hands of the ascendant Taliban gradually became inoperable, but a few flown by the Northern Alliance, which had Russian assistance and access to spares, remained operational up to the US invasion of Afghanistan in late 2001. In 2008, the Afghan Air Force took delivery of six refurbished Mi-35 helicopters, purchased from the Czech Republic. The Afghan pilots were trained by India and began live firing exercises in May 2009 in order to escort Mi-17 transport helicopters on operations in restive parts of the country.

Iran–Iraq War (1980–1988)

[edit]

The Mi-25 saw considerable use by the Iraqi Army during the long war against Iran.[26] Its heavy armament caused severe losses to Iranian ground forces during the war. However, the Mi-25 lacked an effective anti-tank capability, as it was only armed with obsolete 9M17 Skorpion missiles.[27] This led the Iraqis to develop new gunship tactics, with help from East German advisors. The Mi-25s would form "hunter-killer" teams with French-built Aérospatiale Gazelles, with the Mi-25s leading the attack and using their massive firepower to suppress Iranian air defences, and the Gazelles using their HOT missiles to engage armoured fighting vehicles. These tactics proved effective in halting Iranian offensives, such as Operation Ramadan in July 1982.[27]

An Iraqi Mil Mi-25, brought down during the Iran–Iraq War, on display at a military museum in Tehran.

This war also saw the only confirmed air-to-air helicopter battles in history with the Iraqi Mi-25s flying against Iranian AH-1J SeaCobras (supplied by the United States before the Iranian Revolution) on several separate occasions. In November 1980, not long after Iraq's initial invasion of Iran, two Iranian SeaCobras engaged two Mi-25s with TOW wire-guided antitank missiles. One Mi-25 went down immediately, the other was badly damaged and crashed before reaching base.[21][28] The Iranians repeated this accomplishment on 24 April 1981, destroying two Mi-25s without incurring losses to themselves.[21] One Mi-25 was also downed by an IRIAF F-14A.[29]

The Iraqis hit back, claiming the destruction of a SeaCobra on 14 September 1983 (with YaKB machine gun), then three SeaCobras on 5 February 1984[28] and three more on 25 February 1984 (two with Falanga missiles, one with S-5 rockets).[21] A 1982 news article published on the Iraqi Observer claimed an Iraqi Mi-24D shot down an Iranian F-4 Phantom II using its armaments, either antitank missiles, guns or S-5 unguided rockets.[30]

After a lull in helicopter losses, each side lost a gunship on 13 February 1986.[21] Later, a Mi-25 claimed shooting down a SeaCobra with YaKB gun on 16 February, and a SeaCobra claimed downing a Mi-25 with rockets on 18 February.[21] The last engagement between the two types was on 22 May 1986, when Mi-25s shot down a SeaCobra. The final claim tally was 10 SeaCobras and 6 Mi-25s destroyed. The relatively small numbers and the inevitable disputes over actual kill numbers makes it unclear if one gunship had a real technical superiority over the other. Iraqi Mi-25s also claimed 43 kills against other Iranian helicopters, such as Agusta-Bell UH-1 Hueys.[28]

In general, the Iraqi pilots liked the Mi-25, in particular for its high speed, long range, high versatility and large weapon load, but disliked the relatively ineffectual anti-tank guided weapons and lack of agility.[27]

Nicaraguan civil war (1980–1988)

[edit]

Mi-25s were also used by the Nicaraguan Army during the civil war of the 1980s.[31][32] Nicaragua received 12 Mi-25s (some sources claim 18) in the mid-1980s to deal with "Contra" insurgents.[28] The Mi-25s performed ground attacks on the Contras and were also fast enough to intercept light aircraft being used by the insurgents. The U.S. Reagan Administration regarded introduction of the Mi-25s as a major escalation of tensions in Central America.

Two Mi-25s were shot down by Stingers fired by the Contras. A third Mi-25 was damaged while pursuing Contras near the Honduran border, when it was intercepted by Honduran F-86 Sabres and A-37 Dragonflies. A fourth was flown to Honduras by a defecting Sandinista pilot in December 1988.

Sri Lankan Civil War (1987–2009)

[edit]

The Indian Peace Keeping Force (1987–90) in Sri Lanka used Mi-24s when an Indian Air Force detachment was deployed there in support of the Indian and Sri Lankan armed forces in their fight against various Tamil militant groups such as the Liberation Tigers of Tamil Eelam (LTTE). It is believed that Indian losses were considerably reduced by the heavy fire support from their Mi-24s. The Indians lost no Mi-24s in the operation, as the Tigers had no weapons capable of downing the gunship at the time.[28][33]

Since 14 November 1995, the Mi-24 has been used by the Sri Lanka Air Force in the war against the LTTE liberation group and has proved highly effective at providing close air support for ground forces. The Sri Lanka Air Force operates a mix of Mi-24/-35P and Mi-24V/-35 versions attached to its No. 9 Attack Helicopter Squadron. They have recently been upgraded with modern Israeli FLIR and electronic warfare systems. Five were upgraded to intercept aircraft by adding radar, fully functional helmet mounted target tracking systems, and AAMs. More than five Mi-24s have been lost to LTTE MANPADS, and another two lost in attacks on air bases, with one heavily damaged but later returned to service.[33]

Peruvian operations (1989–present)

[edit]

The Peruvian Air Force received 12 Mi-25Ds and 2 Mi-25DU from the Soviets in 1983, 1984, and 1985 after ordering them in the aftermath of 1981 Paquisha conflict with Ecuador. Seven more second hand units (4 Mi-24D and 3 Mi-25D) were obtained from Nicaragua in 1992. These have been permanently based at the Vitor airbase near La Joya ever since, operated by the 2nd Air Group of the 211th Air Squadron. Their first deployment occurred in June 1989 during the war against Communist guerrillas in the Peruvian highlands, mainly against Shining Path. Despite the conflict continuing, it has decreased in scale and is now limited to the jungle areas of Valley of Rivers Apurímac, Ene and Mantaro (VRAEM).[34][35][36]

A Peruvian Mi-35P

Peru also employed Mi-25s against Ecuadorian forces during the short Cenepa conflict in early 1995. The only loss occurred on 7 February, when a FAP Mi-25 was downed after being hit in quick succession by at least two, probably three, 9K38 Igla shoulder-fired missiles during a low-altitude mission over the Cenepa valley. The three crewmen were killed.[37]

By 2011 two Mi-35P were purchased from Russia to reinforce the 211th Air Squadron.[38]

Persian Gulf War (1991)

[edit]
An Iraqi Mi-25 Hind-D, captured during the 1991 Persian Gulf War.

The Mi-24 was also heavily employed by the Iraqi Army during their invasion of Kuwait, although most were withdrawn by Saddam Hussein when it became apparent that they would be needed to help retain his grip on power in the aftermath of the war. In the ensuing 1991 uprisings in Iraq, these helicopters were used against dissidents as well as fleeing civilian refugees.[39][40]

Sierra Leone Civil War (1991–2002)

[edit]

Three Mi-24Vs owned by Sierra Leone and flown by South African military contractors, including Neall Ellis, were used against RUF rebels.[41] In 1995, they helped drive the RUF from the capital, Freetown.[42] Neall Ellis also piloted a Mi-24 during the British-led Operation Barras against West Side Boys.[43] Guinea also used its Mi-24s against the RUF on both sides of the border and was alleged to have provided air support to the LURD insurgency in northern Liberia in 2001–03.

Croatian War of Independence (1990s)

[edit]

Twelve Mi-24s were delivered to Croatia in 1993, and were used effectively in 1995 by the Croatian Army in Operation Storm against the Army of Krajina. The Mi-24 was used to strike deep into enemy territory and disrupt Krajina army communications. One Croatian Mi-24 crashed near the city of Drvar, Bosnia and Herzegovina due to strong winds. Both the pilot and the operator survived. The Mi-24s used by Croatia were obtained from Ukraine. One Mi-24 was modified to carry Mark 46 torpedoes. The helicopters were withdrawn from service in 2004.[44]

First and Second Wars in Chechnya (1990s–2000s)

[edit]

During the First and Second Chechen Wars, beginning in 1994 and 1999 respectively, Mi-24s were employed by the Russian armed forces.

In the first year of the Second Chechen War, 11 Mi-24s were lost by Russian forces, about half of which were lost as a result of enemy action.[45]

Sudanese Civil War (1995–2005)

[edit]

In 1995, the Sudanese Air Force acquired six Mi-24s for use in Southern Sudan and the Nuba mountains to engage the SPLA. At least two aircraft were lost in non-combat situations within the first year of operation. A further twelve were bought in 2001,[46] and used extensively in the oil fields of Southern Sudan. Mi-24s were also deployed to Darfur in 2004–05.

First and Second Congo Wars (1996–2003)

[edit]

Three Mi-24s were used by Mobutu's army and were later acquired by the new Air Force of the Democratic Republic of the Congo.[47] These were supplied to Zaire in 1997 as part of a French-Serbian contract. At least one was flown by Serbian mercenaries. One hit a power line and crashed on 27 March 1997, killing the three crew and four passengers.[48] Zimbabwean Mi-24s were also operated in coordination with the Congolese Army.

The United Nations peacekeeping mission employed Indian Air Force Mi-24/-35 helicopters to provide support during the Second Congo War. The IAF has been operating in the region since 2003.[49]

Kosovo War (1998–1999)

[edit]

Two second-hand Mi-24Vs procured from Ukraine earlier in the 1990s were used by the Yugoslav Special Operation Unit (JSO) against Kosovo Albanian rebels during the Kosovo War.[50]

Insurgency in Macedonia (2001)

[edit]
North Macedonia Mi-24V

The Macedonian military acquired used Ukrainian Mi-24Vs, which were then used frequently against Albanian insurgents during the 2001 insurgency in Macedonia (now North Macedonia). The main areas of action were in Tetovo, Radusha and Aracinovo.[51]

Ivorian Civil War (2002–2004)

[edit]

During the Ivorian Civil War, five Mil Mi-24s piloted by mercenaries were used in support of government forces. They were later destroyed by the French Army in retaliation for an air attack on a French base that killed nine soldiers.[52]

War in Afghanistan (2001–2021)

[edit]
An Afghan Air Force Mi-35 over Kandahar, 2009

In 2008 and 2009, the Czech Republic donated six Mi-24s under the ANA Equipment Donation Programme. As a result, the Afghan National Army Air Corps (ANAAC) gained the ability to escort its own helicopters with heavily armed attack helicopters. ANAAC operates nine Mi-35s. Major Caleb Nimmo, a United States Air Force Pilot, was the first American to fly the Mi-35 Hind, or any Russian helicopter, in combat.[53][54] On 13 September 2011, a Mi-35 of the Afghan Air Force was used to hold back an attack on ISAF and police buildings.[55]

The Polish Helicopter Detachment contributed Mi-24s to the International Security Assistance Force (ISAF). The Polish pilots trained in Germany before deploying to Afghanistan and train with U.S. service personnel. On 26 January 2011, one Mi-24 caught on fire during take-off from its base in Ghazni. One American and four Polish soldiers evacuated unharmed.[56]

India has also donated Mi-35s to Afghanistan. Four helicopters were to be supplied, with three already transferred in January 2016.[57][58][59] The three Mi-35s made a big difference in the offensive against militants, according to General John Campbell, commander of US forces in Afghanistan.[60]

Iraq War (2003–2011)

[edit]

The Polish contingent in Iraq used six Mi-24Ds after December 2004. One of them crashed on 18 July 2006 in an air base in Al Diwaniyah.[61] Polish Mi-24Ds used in Iraq were not returned to Poland due to their age, condition, low combat value of the Mi-24D variant, and high shipping costs; depending on their condition, they were transferred to the new Iraqi Army or scrapped.

War in Somalia (2006–2009) and Somali Civil War (2009–present)

[edit]

The Ethiopian Air Force operated about three Mil Mi-35 and ten Mil Mi-24D helicopter gunships in the Ethiopian invasion of Somalia from 2006 to 2009. One was shot down on 30 March 2007 by Somali insurgents during the Battle of Mogadishu (March–April 2007).[62]

In 2012, three Ugandan Air Force Mi-24s enroute to Somalia to join counterinsurgency operations crashed in Kenya.[63][64] In July 2025, an Mi-24 deployed to support AUSSOM and Somali National Army troops, was destroyed during a crash in Mogadishu.[65][66]

2008 Russo-Georgian War

[edit]

Mil Mi-24s were used by both sides during the fighting in South Ossetia.[67] During the war Georgian Air Force Mi-24s attacked their first targets on an early morning hour of 8 August, targeting the Ossetian presidential palace. The second target was a cement factory near Tskhinvali, where major enemy forces and ammunition were located.[67] The last combat mission of the GAF Mi-24s was on 11 August, when a large Russian convoy, consisting of light trucks and BMP IFVs which were heading to the Georgian village of Avnevi was targeted by Mi-24s, completely destroying the convoy.[67] The Georgian Air Force lost 2 Mi-24s on Senaki air base. They were destroyed by Russian troops on the ground. Both helicopters were in-operational.[68] The Russian army heavily used Mi-24s in the conflict. Russian upgraded Mi-24PNs were credited for destroying 2 Georgian T-72SIM1 tanks, using guided missiles at night time, though some sources attribute those kills to Mil Mi-28.[67] The Russian army did not lose any Mi-24s throughout the conflict, mainly because those helicopters were deployed to areas where Georgian air defence was not active,[67] though some were damaged by small arms fire and at least one Mi-24 was lost due to technical reasons.

War in Chad (2008)

[edit]

On returning to Abeche, one of the Chadian Mi-35s made a forced landing at the airport. It was claimed that it was shot down by rebels.[69][70]

Libyan civil war (2011)

[edit]
A Libyan Air Force Mil Mi-35

The Libyan Air Force Mi-24s were used by both sides to attack enemy positions during the 2011 Libyan civil war.[71] A number were captured by the rebels, who formed the Free Libyan Air Force together with other captured air assets. During the battle for Benina airport, one Mi-35 (serial number 853), was destroyed on the ground on 23 February 2011. In the same action, serial number 854 was captured by the rebels together with an Mi-14 (serial number 1406).[citation needed] Two Mi-35s operating for the pro-Gaddafi Libyan Air Force were destroyed on the ground on 26 March 2011 by French aircraft enforcing the no-fly zone.[72] One Free Libyan Air Force Mi-25D (serial number 854, captured at the beginning of the revolt) violated the no-fly-zone on 9 April 2011 to strike loyalist positions in Ajdabiya. It was shot down by Libyan ground forces during the action. The pilot, Captain Hussein Al-Warfali, died in the crash.[citation needed] The rebels claimed that a number of other Mi-25s were shot down.

2010–2011 Ivorian crisis

[edit]

Ukrainian army Mi-24P helicopters as part of the United Nations peacekeeping force fired four missiles at a pro-Gbagbo military camp in Ivory Coast's main city of Abidjan.[73]

Syrian Civil War (2011–2024)

[edit]

The Syrian Air Force has used Mi-24s during the ongoing Syrian Civil War, including in many of the country's major cities.[74] Controversy has surrounded an alleged delivery of Mi-25s[by whom?] to the Syrian military, due to Turkey and other NATO members disallowing such arms shipments through their territory.[vague][75]

On 3 November 2016, a Russian Mi-35 made an emergency landing near Syria's Palmyra city, and was hit and destroyed, most likely by an unguided recoilless weapon after it touched down. The crew returned safely to the Khmeimim air base.[76]

Second Kachin conflict (2011–present)

[edit]

The Myanmar Air Force used the Mi-24 in the Kachin conflict against the Kachin Independence Army.[77] Two Mi-35 helicopters were shot down by the Kachin Independence Army during the heavy fighting in the mountains of northern Burma in 2012 and early 2013.[78]

On 3 May 2021, in the morning, a Myanmar Air Force Mi-35 was shot down by the Kachin Independence Army, hit by a MANPADS during air raids involving attack helicopters and fighter jets. A video emerged showing the helicopter being hit while flying over a village.[79][80]

Post-U.S. Iraqi insurgency

[edit]

Iraq ordered a total of 34 Mi-35Ms in 2013, as part of an arms deal with Russia that also included Mi-28 attack helicopters.[81] The delivery of the first four was announced by then-Prime Minister Nuri al-Maliki in November 2013.[82][83]

Their first deployment began in late December against camps of the al-Qaeda linked Islamic State of Iraq and the Levant (ISIL) and several Islamist militants in the al-Anbar province that had taken control of several areas of Fallujah and Ramadi.[84] FLIR footage of the strikes has been released by the military.[85]

On 3 October 2014, ISIL militants reportedly used a FN-6 shoulder-launched missile in Baiji to shoot down an Iraqi Army Mi-35M attack helicopter.[86] Video footage released by ISIL militants shows at least another two Iraqi Mi-35s brought down by light anti-aircraft artillery.[87]

Balochistan Insurgency (2012–present)

[edit]

In 2018, Pakistan received 4 Mi-35M Hind-E Gunships from Russia under the $153 million deal.[88][89] They are now stationed at the Army Aviation Corps base at Quetta Cantonment. The gunships have since been used in several counter insurgency operations against various militant groups in the Balochistan province of Pakistan. In early 2022, a base in Nushki and a check-post in Panjgur belonging to the Frontier Corps Balochistan Paramilitary were attacked by BLA terrorists. The attack in Nushki was swiftly repulsed but the situation in Panjgaur was not good to which Mi-35 Hind and AH-1F Cobra gunships were called in for support. It provided much needed ground support and reconnaissance in the counter offensive which led to success.[90][91]

Russian annexation of Crimea (2014)

[edit]

During the annexation of Crimea by the Russian Federation, Russia deployed 13 Mi-24s to support their infantry as they advanced through the region. However these aircraft saw no combat during their deployment.[92]

War in Donbas (2014-2022)

[edit]
Ukrainian Mil Mi-24 during training at the time of the war in Donbas

During the Siege of Sloviansk, on 2 May 2014, two Ukrainian Mi-24s were shot down by pro-Russian insurgents. The Ukrainian armed forces claim that they were downed by MANPADS while on patrol close to Sloviansk.[93] The Ukrainian government confirmed that both aircraft were shot down, along with an Mi-8 damaged by small arms fire. Initial reports mentioned two dead and others wounded; later, five crew members were confirmed dead and one taken prisoner until being released on 5 May.[94][95][96]

On 5 May 2014, another Ukrainian Mi-24 was forced to make an emergency landing after being hit by machine gun fire while on patrol close to Sloviansk. The Ukrainian forces recovered the two pilots and destroyed the helicopter with a rocket strike by an Su-25 aircraft to prevent its capture by pro-Russian insurgents.[97]

Ukrainian Su-25s, with MiG-29 fighters providing top cover, supported Mi-24s during the battle for Donetsk Airport.[98]

On 13 October 2018, a Ukrainian Mi-24 shot down an Orlan-10 UAV using cannon fire near Lysychansk.[99]

Chadian offensive against Boko Haram (2015)

[edit]

Chadian Mi-24s were used during the 2015 West African offensive against Boko Haram.[100]

Azerbaijan-Karabakh (2014–2016, 2020)

[edit]

On 12 November 2014, Azerbaijani forces shot down an Armenian forces Mi-24 from a formation of two which were flying along the disputed border, close to the frontline between Azerbaijani and Armenian troops in the disputed Karabakh territory. The helicopter was hit by an Igla-S shoulder-launched missile fired by Azerbaijani soldiers while flying at low altitude and crashed, killing all three on board.[101][102][103]

On 2 April 2016, during a clash between Azerbaijani and Armenian forces, an Azerbaijani Mi-24 helicopter was shot down by "Nagorno-Karabakh" forces. The downing was confirmed by the Azerbaijani defence ministry.[104][105][106][107]

On 9 November 2020, during the Nagorno-Karabakh war a Russian Mi-24 was shot down by Azerbaijani forces with a MANPADS.[108] The Azerbaijan Foreign Ministry stated that the downing was an accident. Two crew members were killed and one sustained moderate injuries. The Russian defence ministry confirmed the downing in a press release the same day.[109]

Russian invasion of Ukraine (2022–present)

[edit]

During the 2022 Russian invasion of Ukraine, both Ukraine and Russia have used Mi-24 helicopters. On 1 March 2022, Ukrainian forces shot down a Russian Mi-35M helicopter with MANPADS, in the Kyiv Reservoir (see also Battle of Kyiv). On 5 May 2022, the helicopter was retrieved by Ukrainian engineers in Vyshgorod.[110] Two Russian Mi-35 were shot down by a MANPADS on 5 March 2022.[111][112] On 6 March, one Mi-24P with registration number RF-94966 was shot down by Ukrainian MANPADS in Kyiv Oblast.[113][114] On 8 March 2022 one Ukrainian Mil Mi-24 from the Ukrainian 16th Army Aviation Brigade [uk] was lost over Brovary, Kyiv. Pilots Col. Oleksandr Maryniak and Cptn. Ivan Bezzub were killed.[115][116] On 17 March a Russian Mi-35M was reported destroyed by Ukrainian Ministry of Defence, unknown location.[117] On 1 April 2022, two Ukrainian Mi-24s reportedly entered Russia and attacked an oil storage facility in Belgorod.[118]

In May 2022, the Czech Republic donated Mi-24 helicopters to Ukraine.[119] In July 2023, it was reported that Poland secretly donated at least a dozen Mi-24s to Ukraine.[120] In late 2023, Russia tried to buy the deactivated Mi-35 from the Brazilian Air Force, but the Brazilian government denied the sale.[121]

As of 27 May 2025, visually confirmed losses compiled by Oryx blog are listed as following: 4 Mi-24P, 4 Mi-24V/P/35M, 10 Mi-35M for the Russian side, and 2 Mi-24P and 7 Mi-24 of unknown variant for the Ukrainian side.[122]

Variants

[edit]

Operators

[edit]
Operators
  Current
  Former
 Afghanistan
 Algeria
Angola
 Armenia
 Azerbaijan
 Belarus
Brazilian Air Force Mi-35M
A Bulgarian Air Force Mi-24 in flight
 Bulgaria
Burkina Faso
 Burundi
Chad
Congo, Republic of the
 Democratic Republic of the Congo
 Cuba
A Czech Air Force Mi-24
 Djibouti
Egypt
Eritrea
Ethiopia
Georgian Air Force Mi-24
Georgia
Guinea
Hungarian Mi-24
 Hungary
India
 Indonesia
An AH-64E Apache Guardian, and a Mi-35 from Indonesian Army
Iraq
Kazakhstan
Kyrgyzstan
 Libya
Mali
Mozambique
  • Mozambique Air Force - 2 Mi-25 as of 2023[148]
 Myanmar
Namibia
Nigerian Air Force Mil Mi-24V
 Niger
Nigeria
 Pakistan
Peruvian Air Force Mi-25D
 Peru
 Poland
A Russian Air Force Mil Mi-35P
 Russia
Rwanda
Serbian Mil Mi-35M during Sadejstvo 2020 military exercise
Serbia
Senegal
Sierra Leone
Sri Lanka
Sudan
Syria
Tajikistan
Turkmenistan
Uganda People's Defence Force Air Wing Mil Mi-24V
Uganda
 Ukraine
 United States
Uzbekistan
Venezuela
Yemen
Zimbabwe

Former operators

[edit]
 Armenia
 Brazil
Croatia
Cyprus
Czech Republic
Czechoslovakia

Czechoslovak Air Force[173][174]

Equatorial Guinea

Equatorial Guinean Air Force[173]

East Germany
Germany
Kampuchea
 Nicaragua
North Macedonia
Slovakia
South Yemen
Vietnam People's Air Force Mi-24
Soviet Union
Yugoslavia
Transnistria
Vietnam

Possible operators

[edit]
 North Korea

Aircraft on display

[edit]

Mi-24 helicopters can be seen in the following museums:

Russia Central Air Force Museum, Monino – Mi-24A, Mi-25
Belgium Royal Museum of the Armed Forces and Military History, Brussel – Mi-24
Brazil Museu Aeroespacial, Rio de Janeiro – Mi-35M
Bulgaria
Czech Republic Prague Aviation Museum, Kbely – Mi-24D tactical number 0220
China Chinese Aviation Museum, Beijing – Mi-24
Denmark Panzermuseum East, SlagelseEast-German Mi-24P Hind-F from 1989 (construction nr.: 340339). Assigned NVA s/n 464, later German Army s/n 96+49.[citation needed]
Ethiopia Martyrs Memorial Monument, Bahir Dar - Mi-24A[190]
Germany
Hungary
Iran Sa'ad Abad Museum in Tehran
Latvia Riga Aviation Museum, Riga – Mi-24A tactical number 20
Nicaragua Airforce Base Augusto C. Sandino International Airport, Managua, Mi-25 tactical number 361
Poland
South Africa South African Air Force Museum, Swartkops Air Force Base – One Mi-24A of the Algerian Air Force on display.
Slovakia Military History Museum, Piešťany – Mi-24D tactical number 0100[191]
Sri Lanka
Ukraine
United Kingdom
United States
Vietnam

Specifications (Mi-24)

[edit]
Orthographic projection of the Mil Mi-24.
Orthographic projection of the Mil Mi-24.
Cabin door to the rear troop-utility compartment
Possible armament configuration on Mi-24W
Yakushev-Borzov YakB-12.7 machine gun
Mi-24 during "Centre 2019" exercise

Data from Indian-Military.org[198][unreliable source?]

General characteristics

  • Crew: 2 pilots, 1 weapons system officer and 1 technician (optional)
  • Capacity: 8 troops / 4 stretchers / 2,400 kg (5,291 lb) cargo on an external sling
  • Length: 17.5 m (57 ft 5 in) fuselage only
19.79 m (65 ft) including rotors
  • Wingspan: 6.5 m (21 ft 4 in) stub wings
  • Height: 6.5 m (21 ft 4 in)
  • Empty weight: 8,500 kg (18,739 lb)
  • Max takeoff weight: 12,000 kg (26,455 lb)
  • Powerplant: 2 × Isotov TV3-117 turboshaft engines, 1,600 kW (2,200 shp) each
  • Main rotor diameter: 17.3 m (56 ft 9 in)
  • Main rotor area: 235.1 m2 (2,531 sq ft) NACA 23012[199]

Performance

  • Maximum speed: 335 km/h (208 mph, 181 kn)
  • Range: 450 km (280 mi, 240 nmi)
  • Ferry range: 1,000 km (620 mi, 540 nmi) [citation needed]
  • Service ceiling: 4,900 m (16,100 ft)
  • Rate of climb: 12.2 m/s (2,400 ft/min) MI-24A

Armament

Internal guns
  • flexible 12.7 mm Yakushev-Borzov Yak-B Gatling gun on most variants with a maximum of 1,470 rounds of ammunition
  • fixed twin-barrel GSh-30K autocannon on the Mi-24P with 250 rounds of ammunition.
  • flexible twin-barrel GSh-23L autocannon on the Mi-24VP, Mi-24VM and Mi-35M with 450 rounds
  • flexible GIAT dual feed 20mm (M693) autocannon on Mi-24 SuperHind Mk.II/III/IV/V with 320 rounds
  • PKB passenger compartment window mounted machine guns
External stores
  • Total payload claimed is up to 2,400 kg of external stores from Mi-24P (Russians typically claim 2,400 kg like link in first ref but link in second ref claims 2,500).[200][201]
  • Inner hardpoints can carry at least 500 kg.
  • Outer hardpoints can carry at least 500 kg when carrying PTB-450 450 litre fuel tanks (fuel weight up to 378 kg except empty tank weight), or B-8V20 rocket pod with S-8 (rocket) that weigh over 400 kg when fully loaded with HE-FRAG-Delayed rounds for anti-armor roles (20 round loaded weight including pod is 457 kg) or the lighter Anti-Concrete rocket (20 round loaded weight including pod is 427 kg).[202] 4 × R-60 AIM - 2 per each 4 pylons. Also can be loaded under wingtips but cannot find any pictures or records that R-60M being fired from wingtip.
  • Wing-tip pylons can only carry the 9M17 Phalanga (in the Mi-24A-D), the 9K114 Shturm complex (in the Mi-24V-F) per each side.
Bomb load
  • Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), up to 500 kg
  • MBD multiple ejector racks (presumably MBD-4 with 4 × FAB-100)
  • KGMU2V submunition/mine dispenser pods
First-generation armament (standard production Mi-24D)
Second-generation armament (Mi-24V, Mi-24P and most upgraded Mi-24D)
  • UPK-23-250 gunpod carrying the GSh-23L
  • B-8V20 a lightweight long tubed helicopter version of the S-8 rocket launcher
  • 9K114 Shturm in pairs on the outer and wingtip pylons
Anti-Air missiles
Both can be carried as either one or two per pylon.
[edit]

The Mi-24 has appeared in several films and has been a common feature in many video games.

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

References

[edit]

Further reading

[edit]
[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia

The Mil Mi-24 (NATO reporting name Hind), known to Soviet pilots as the "flying tank" (letayushiy tank), is a large helicopter gunship, attack helicopter, and low-capacity troop transport developed by the Mil Moscow Helicopter Plant in the Soviet Union during the mid-1960s, with its first flight occurring on 19 September 1969 and entry into service in 1972-1973. Designed to fulfill a requirement for an armored, heavily armed platform capable of both close air support and transporting up to eight troops or equivalent cargo, it features a crew of two (pilot and weapons systems operator), twin Klimov TV3-117 turboshaft engines providing up to 2,200 horsepower each, a maximum speed of approximately 330 km/h, and armament including anti-tank guided missiles, rocket pods, bombs, and a chin-mounted machine gun or, in variants like the Mi-24P, a 30 mm cannon across multiple hardpoints. Over 3,000 units have been produced, with variants such as the Mi-24D, Mi-24V, and export Mi-35 continuing to serve in more than 40 countries, including Russia, India, Iraq, and Libya.
The Mi-24's defining characteristics include its heavily armored fuselage capable of withstanding small-arms fire and shrapnel, stub wings for weapon pylons, and a spacious cabin that distinguishes it from dedicated Western attack helicopters like the AH-64 , enabling rapid insertion under fire—a concept rooted in Soviet doctrine emphasizing operations. Its combat debut came in the 1977 between and , followed by extensive use in the Soviet-Afghan War (1979-1989), where it demonstrated formidable firepower against ground targets but revealed vulnerabilities to man-portable air-defense systems like the , leading to significant losses and subsequent upgrades in countermeasures and tactics. Iraqi Mi-24s achieved notable successes during the Iran-Iraq War (1980-1988), including downing Iranian AH-1 Cobra helicopters and F-4 Phantom jets, underscoring the platform's anti-air and anti-armor capabilities when operated effectively. Despite its age, modernized versions like the Mi-35M incorporate advanced avionics, night-vision systems, and improved engines, ensuring ongoing relevance in conflicts such as those in , , and , where its ruggedness and capacity provide advantages in austere environments over lighter, less versatile alternatives.

Development

Design Origins and Requirements

The Mil Mi-24 originated from Soviet military requirements in the mid-1960s for a multi-role helicopter combining troop transport with heavy fire support, reflecting doctrinal emphasis on rapid infantry insertion and suppression of enemy armor and positions in mechanized warfare. This concept diverged from U.S. practices observed in Vietnam, where transport (e.g., UH-1 Huey) and attack (e.g., AH-1 Cobra) roles were separated; Soviet planners insisted on a single platform to carry eight combat-ready troops alongside substantial armament, enhancing operational flexibility for airborne assaults. In 1965, Mikhail Mil, head of the design bureau, proposed developing an armored dedicated to and functions, armed with integrated weapons to provide direct support during troop deployment. Drawing from experience with Mi-8 transports experimentally fitted as gunships, the design addressed needs for survivability in contested environments, including protection against small-arms fire and the ability to operate in diverse terrains. The Soviet Ministry of Defense formalized the requirement on May 6, 1968, specifying a twin-turboshaft helicopter with a crew of two, troop capacity for eight, external pylons for rockets and guided missiles, and a fuselage layout prioritizing armor plating and a low-profile for reduced vulnerability. Key performance goals included cruise speeds exceeding 250 km/h, operational range of approximately 450 km, and integration of a nose-mounted gun for close support, all to fulfill the role of an airborne equivalent to ground-based infantry fighting vehicles. The V-24 project, approved in 1967 following mockup reviews, incorporated Mi-8-derived engines and rotors adapted for heavier combat loads, underscoring the priority of firepower and endurance over pure transport efficiency.

Prototyping and Initial Testing

The Mil Mi-24's prototyping originated from Soviet military requirements in the mid-1960s for a combined troop transport and , with Mikhail Mil's design bureau receiving approval to develop a around 1967. The initial design, designated V-24, incorporated armored protection for up to eight troops alongside capabilities, drawing from the Mi-8's but with a narrower profile and enhanced armament provisions. By February 1969, the Soviet Ministry of Defense formally endorsed the Mil bureau's proposal over competitors, prioritizing its multi-role integration of transport and attack functions. The first V-24 prototype rolled out in June 1969, powered by TV2-117 engines and featuring a five-bladed main rotor. Ground and tethered hover tests commenced on September 15, 1969, at the Mil airfield near , evaluating stability, vibration, and basic systems integration under controlled conditions. Four days later, on September 19, 1969, test pilot conducted the maiden untethered flight, lasting several minutes and confirming initial handling qualities without major anomalies. This rapid progression from rollout to flight—spanning less than four months—reflected the Mil bureau's iterative approach, leveraging data and subscale models to minimize risks in rotor dynamics and armor weight distribution. Subsequent initial testing expanded to a series of 12 prototypes, which underwent factory trials focusing on flight envelope expansion, engine performance under load, and weapons integration feasibility. Early flights revealed challenges with center-of-gravity shifts due to troop compartment ballast and rotor efficiency at high speeds, prompting minor airframe adjustments by late 1969. A second prototype followed shortly, incorporating refined avionics and stub-wing hardpoints for rocket pods, with tests validating short takeoff and landing capabilities essential for assault operations. By 1970, pre-production evaluation units were delivered to Soviet Army aviation units for operational trials, assessing survivability in simulated combat environments and troop deployment efficiency, though full state acceptance trials extended into 1971-1972 to address vibration-induced fatigue in the armored cockpit.

Production and Entry into Service

The Mil Mi-24 transitioned to serial production after formal acceptance by Soviet military authorities, with the initial Mi-24A variant entering service with the Soviet Air Force in 1972. This early production model, designated Hind-A by NATO, featured a greenhouse-style cockpit enclosing both crew members and troops, and was powered by TV2-117 turboshaft engines. Manufacturing occurred primarily at the Mil Moscow Helicopter Plant, with the first units delivered for operational evaluation as early as 1970. Production of the Mi-24A continued from 1970 to 1972, yielding the initial batch of operational helicopters before refinements led to subsequent variants. The Mi-24D, an interim gunship version with a redesigned nose for improved pilot visibility, entered production in 1973 at the Arsenyev and Rostov-on-Don plants, with approximately 350 units completed by 1977. These early models established the Mi-24's role as a multi-purpose combat helicopter, capable of transporting up to eight troops while providing fire support, though initial deployments revealed limitations in night operations and vulnerability to small-arms fire that prompted later modifications. By the mid-1970s, the type had become a staple of Soviet tactical aviation units, with production scaling to support widespread deployment across Warsaw Pact forces.

Modernization and Upgrade Programs

The Mil Mi-24 has been subject to extensive modernization programs by and various operator nations to extend , improve , and integrate modern and weaponry. These upgrades address limitations in night operations, targeting precision, and countermeasures against advanced threats, often involving replacement of obsolete systems with digital interfaces and enhanced sensors. In , the Mi-35M, developed as a deep modernization of the Mi-24V, features engines each rated at 2,200 kW (2,950 shp), providing superior hot-and-high performance compared to the original TV3-117 engines. It incorporates a new four-blade main rotor with composites for reduced vibration and improved lift, shortened stub wings for better maneuverability, and the OPS-24N electro-optical targeting system enabling all-weather, day-night target acquisition up to 10 km. Armament upgrades include compatibility with anti-tank missiles, Igla-V air-to-air missiles, and unguided rockets, while the cockpit supports night-vision goggles and features armored glass. The variant entered production in 2005, with deliveries to the commencing around 2010. Further Russian efforts include the Mi-24PN, a night-capable upgrade of the Mi-24P introduced in the early , featuring a Panoramic (PNVD-24) and four-channel TV/thermal imaging for low-light operations. In August 2024, unveiled the Mi-24P-1M at the Army-2024 forum, integrating the President-S system, upgraded optics for enhanced detection range, and reinforced pilot protection against small arms fire. Internationally, South Africa's Advanced Technologies & Engineering (ATE) developed the SuperHind program in the , reducing empty weight by nearly 2 tons through structural modifications, replacing the chin turret with a South African-developed 20mm , and adding Western for improved fire control and navigation. pursued Mi-24 upgrades from 2019, focusing on new weaponry integration, digital cockpits, and compatibility with systems to bridge capability gaps pending new platforms. offers a modular package for Mi-24/35 fleets, including glass cockpits, (FLIR), and electronic warfare suites for day/night missions. Ukraine's modernization incorporates , thermal imagers, and indigenous TV3-117VMA-SBM1 engines for enhanced reliability. These programs reflect operator-specific adaptations, prioritizing cost-effective enhancements over full replacements.

Design Features

Airframe Construction and Survivability Measures

The Mil Mi-24 features an all-metal semi-monocoque fuselage consisting of a pod-and-boom structure, primarily constructed from aluminum alloys for the main body, with steel and titanium incorporated in critical areas for strength and protection. The five-blade main rotor utilizes constant-chord blades with aluminum alloy spars, skins, and honeycomb cores, while the three-blade tail rotor is made of aluminum alloy; later variants reinforced the rotor system with titanium to enhance durability against impacts. Fixed shoulder-mounted wings of all-metal construction provide additional lift and hardpoints without movable control surfaces. Survivability is prioritized through extensive ballistic armor, enabling operations in high-threat environments. The fuselage incorporates 5 mm hardened steel plating along the front sides and around the engines to deflect small arms fire and fragments. The crew stations are housed in a titanium-armored tub, complemented by armored seats for the pilot and weapon operator, optically flat bulletproof glass windscreens, and an anti-fragment shield between cockpits, collectively designed to resist 12.7 mm rounds from multiple angles. The cockpit and crew compartment maintain overpressurization to guard against chemical, biological, radiological, and nuclear contaminants. Nitrogen-pressurized spars in the rotors facilitate crack detection, and hydraulic lead-lag dampers on the main rotor mitigate vibration-induced damage. Later models integrated enhanced countermeasures tied to airframe resilience, including warning receivers, jammers, and flare/chaff dispensers to evade missiles, alongside exhaust suppressors to reduce . These measures, combined with the robust , allow the Mi-24 to withstand hits from 20 mm cannon fire in key components like the reinforced rotors, though vulnerability persists to larger calibers and man-portable air-defense systems without active evasion.

Propulsion System and Flight Performance

The Mil Mi-24 is powered by two engines mounted above the , each rated at approximately 2,200 shaft horsepower (shp) for takeoff, with variants like the TV3-117V providing up to 2,225 shp. These engines drive a five-bladed main rotor with a of 17.3 meters and a three-bladed , enabling the helicopter's combined and transport roles through efficient power distribution. The TV3-117 series features dust-resistant intakes and high-altitude adaptations, contributing to operational reliability in diverse environments, though early models experienced occasional powerplant overheating under heavy loads. Flight performance emphasizes speed and maneuverability over pure hovering endurance, with a maximum speed of 335 km/h at and a typical cruise speed of 280–295 km/h. The stub wings, with a sweep of 8.5 degrees and area of 6.25 , generate supplemental lift equivalent to about 20–25% of total lift at high speeds, reducing rotor loading and enabling dash capabilities up to 320–335 km/h while carrying payloads. Service ceiling reaches 4,500–4,600 meters, with a hover ceiling out of ground effect at around 2,200 meters under standard conditions. Operational range varies by configuration: internal fuel provides 450–500 km with a combat load, extending to 950–1,050 km on ferry missions with auxiliary tanks. Climb rate stands at approximately 15 m/s, supporting rapid ingress in assault scenarios, though fuel consumption increases markedly above 250 km/h due to the engines' flat-rated power curve.
ParameterValue
Maximum Speed335 km/h
Cruise Speed280–295 km/h
Service 4,500–4,600 m
Hover (OGE)2,200 m
Range (Combat Load)450–500 km
Ferry Range950–1,050 km
(each)2,200–2,225 shp

Crew Stations, Avionics, and Defensive Systems

The Mil Mi-24 employs a of two: a pilot and a gunner/weapons systems (WSO). Early variants, such as the Mi-24A, featured a stepped side-by-side layout with the pilot seated slightly higher and offset to the rear for improved visibility, protected by armored glazing capable of withstanding 12.7 mm rounds. From the Mi-24D model introduced in 1973, a configuration became standard, positioning the gunner in the forward for targeting focus and the pilot aft, enhancing streamlining and while maintaining armored protection against small arms fire. Both stations include overpressurization for nuclear, biological, and chemical () defense, with ergonomic designs prioritizing survivability and control accessibility. Avionics in the baseline Mi-24 series rely on analog suited for low-altitude operations, including a gyro horizon, magnetic compass system, radio altimeter, and identification friend-or-foe (IFF) interrogator. Communication systems comprise R-860 or R-863 VHF , R-863M HF , and R-818 UHF sets for coordination with ground forces. Navigation aids feature the ARK-15M or ARK-22 (ADF), GP-1 , and (), enabling all-weather flight and precise targeting integration with the GOES-342 electro-optical sight in later models. Upgrades in export and modernized variants, such as the Mi-35M, incorporate glass cockpits with multifunction displays, helmet-mounted sights, and digital autopilots for goggle (NVG) compatibility and reduced pilot workload. Defensive systems emphasize passive and active countermeasures developed from combat feedback, particularly Soviet experiences in starting in 1979, where man-portable air-defense systems (MANPADS) inflicted significant losses. Standard equipment includes the SPO-10 (RWR) for threat detection and the ASO-2V dispenser launching and (IR) flares to decoy missiles. Optional enhancements feature directional IR jammers like the President-S in three-turret configurations to disrupt heat-seekers, alongside armored vital zones shielding engines, fuel tanks, and cockpits from 20-23 mm projectiles. These measures, combined with low-level flight tactics, improve survivability, though effectiveness varies against advanced threats without comprehensive electronic warfare suites found in Western counterparts.

Armament, Payload Capacity, and Multi-Role Integration

The Mil Mi-24 features a flexible armament suite designed for anti-armor, , and suppression roles, centered on a chin-mounted and multiple underwing hardpoints for suspended ordnance. Early like the Mi-24A and Mi-24D typically mount a 12.7 mm Yak-B four-barrel with 1,470 rounds, while later models such as the Mi-24P incorporate a fixed 30 mm GSh-30K twin-barrel cannon or 23 mm GSh-23L turreted guns for enhanced firepower against ground targets. Suspended weapons are carried on four to six hardpoints (two to three per stub wing), enabling configurations for up to 1,500 kg of external ordnance including anti-tank guided missiles, pods, and bombs. Common anti-tank options include up to eight 9M114 Shturm (AT-6 Spiral) or (AT-9) missiles with ranges of 5–8 km and warheads capable of penetrating 650–800 mm of armor, supplemented by S-5 57 mm in UB-16 or UB-32 pods, S-24 unguided , FAB-100/250 free-fall bombs, or gun pods like the UPK-23 with twin 23 mm cannons.
Weapon TypeExamplesCapacity per Sortie
Anti-Tank Missiles9M114 Shturm / Up to 8 missiles
Rocket PodsS-5 (UB-16/32), S-24Multiple pods per
BombsFAB-100, 1–4 units with racks
Other dispensers, grenade launchersVariable pods
Payload capacity supports a of 11.5–12 tons, with internal cargo limited to 8 combat-equipped troops or 4 litters in the armored cabin, and external sling loads reaching 2,500 kg when unburdened by weapons. This allows for 1,500 kg dedicated to armaments or auxiliary fuel tanks up to 1,200 kg total, though full troop loads reduce available ordnance due to weight constraints. Multi-role integration stems from the Mi-24's hybrid design, combining lethality with light in a single , enabling small-unit insertion under fire via the troop bay's side-firing ports for suppressive small-arms fire. The configuration permits simultaneous carriage of 8 troops and anti-tank missiles or rockets, facilitating rapid deployment of or infantry squads for seizure of key terrain, though operational doctrine often prioritizes attack over to maximize radius and . This duality enhances tactical flexibility in contested environments but imposes trade-offs, as troops occupy space otherwise usable for or munitions, limiting endurance compared to dedicated platforms.

Combat Capabilities

Gunship and Close Air Support Effectiveness

The Mil Mi-24 excels in and roles through its armored airframe, which permits low-altitude operations under fire, combined with a capacity exceeding 1,500 kg of munitions including unguided rockets, cannon pods, bombs, and anti-tank guided missiles such as the 9M114 Shturm (AT-6 Spiral). This configuration enables suppression of infantry, destruction of light vehicles, and engagement of armored targets at ranges up to 5 km for missiles, with the AT-6 achieving a reported kill ratio exceeding 90% in tested conditions. Crew survivability is enhanced by armor shielding vital areas, allowing the helicopter to withstand small-arms fire and shrapnel, though it remains vulnerable to dedicated anti-aircraft systems. In the Soviet-Afghan War (1979–1989), the Mi-24 proved highly effective for , conducting thousands of sorties to protect convoys, support ground sweeps, and strike Mujahedin positions, often operating in pairs or flights of four to eight for mutual defense. Tactics included low-level "wheel of death" circular attacks with 80 mm S-8 rockets and 23 mm gun pods, as well as night operations using illumination flares, which terrorized insurgents and disrupted ambushes effectively prior to widespread MANPADS proliferation. By 1983, Soviet forces deployed up to 200 Mi-24s in theater, forming the backbone of rotary-wing despite harsh high-altitude conditions limiting full payloads. The introduction of FIM-92 Stinger missiles in 1986 challenged Mi-24 dominance, with initial losses prompting shifts to higher-altitude standoff attacks and infrared countermeasures like flares, reducing effectiveness against fleeting targets but sustaining operational viability through 1989. Total Mi-24 losses reached 333 over the conflict, mostly to ground fire, yet the platform's contributed decisively to tactical successes in suppressing resistance and enabling advances. In export conflicts such as Angola's , Mi-24s provided analogous CAS against South African incursions, leveraging similar tactics to neutralize ground threats. Limitations include reduced maneuverability compared to lighter attack helicopters, with a top speed of 335 km/h and constraining hover stability under load, occasionally necessitating reduced armament for hot-and-high . Nonetheless, upgrades like night-vision compatibility and improved missiles have sustained its in contemporary low-intensity operations, where armor and volume of fire outweigh agility for CAS against irregular forces.

Troop Transport and Assault Role

The Mil Mi-24 was designed with an integrated troop compartment in its central fuselage, enabling it to transport up to eight fully equipped soldiers alongside its armament and crew, distinguishing it from dedicated attack helicopters like the AH-64 Apache. This configuration supported Soviet doctrine for "flying infantry fighting vehicles," where the helicopter could suppress enemy positions with onboard weapons—such as 12.7 mm machine guns, rocket pods, or anti-tank missiles—while landing troops for immediate assault, followed by extraction under covering fire. The compartment featured armored seating, access via rear ramps or side doors, and provisions for securing small cargo up to 1.5 tonnes as an alternative to personnel, allowing flexibility in air assault operations. In practice, the Mi-24's assault role emphasized rapid insertion into contested areas, with the crew's elevated piloting and gunner stations providing visibility for coordinating during hover or low-speed maneuvers. Operational doctrine prioritized tactics, where Mi-24s would precede larger Mi-8 transports, neutralizing anti-air threats and ground defenses to enable troop debarkation within minutes. However, performance constraints, including reduced lift in high-altitude or hot environments—limiting payload to fewer than eight troops at elevations above 2,000 meters—often rendered the transport function secondary to gunship duties, with Soviet forces favoring dedicated Mi-8s for primary troop lifts. Export operators, such as those in Middle Eastern and African conflicts, adapted the Mi-24 more variably for , leveraging its armor and firepower for small-unit raids or insertions, though the cramped compartment (approximately 2.5 meters long) restricted prolonged troop carriage or medical evacuations compared to purpose-built transports. Upgraded variants like the Mi-35 retained this capability with enhanced for night s, but empirical data from engagements indicate the role's effectiveness hinged on low-threat environments, where the helicopter's 335 km/h cruise speed facilitated surprise over sustained transport hauls. Overall, while innovative, the Mi-24's hybrid design achieved tactical integration at the cost of optimized specialization in either transport or attack.

Vulnerabilities and Tactical Limitations

The Mil Mi-24's substantial dimensions and mass, exceeding 8,000 kg in combat configuration, compromised its agility compared to lighter attack helicopters, rendering it a larger target during low-altitude operations essential for . This design prioritized armored protection against 12.7 mm rounds but limited evasive maneuvers, with banking beyond 37 degrees in turns often irrecoverable due to stability constraints. In high-altitude environments like Afghanistan's , thin air reduced engine power output and rotor lift, necessitating the removal of troop compartment armor to maintain performance, though this exposed embarked personnel to greater risk. Dusty conditions further exacerbated engine wear, prompting retrofits with particle separators after initial deployments revealed rapid degradation. Susceptibility to man-portable air-defense systems (MANPADS) emerged as a critical vulnerability, particularly infrared-homing missiles exploiting the helicopter's prominent engine exhaust signatures. During the Soviet-Afghan War (1979–1989), early losses totaled around 5% to small arms and unguided rockets like the SA-7, but the 1986 introduction of U.S.-supplied FIM-92 Stingers escalated attrition, with approximately 140 confirmed hits from 187 launches between September 1986 and August 1987 alone, contributing to 333 total Mi-24 losses per Soviet records. Tactical responses included erratic flight paths, reduced loiter times, and adoption of infrared flares by 1989, yet these measures curtailed operational tempo and effectiveness against ground threats at altitudes above 1,500–2,000 feet where MANPADS engagement envelopes peaked. The Mi-24's main rotor assembly also proved fragile to rifle-caliber impacts, enabling mujahideen marksmen to disable aircraft through precise shots despite armored vital areas. Tactically, the dual-role concept strained the platform's capabilities, as carrying up to eight troops reduced for munitions, range, and speed, often rendering the transport function secondary or abandoned in favor of pure missions to avoid divided attention during engagements. Rearward visibility limitations in variants like the Mi-24D created blind spots exploitable by trailing threats, while early models lacked robust night-vision or navigation aids, confining operations to daylight and increasing exposure to ambushes. High maintenance demands, averaging 2–9 hours per flight hour in austere conditions, further limited rates and sustained availability, amplifying logistical burdens in prolonged conflicts. These factors collectively favored over persistent hovering, underscoring the Mi-24's reliance on standoff weapons and escorts for survival against adaptive insurgents.

Operational History

Initial Combat Deployments (1970s)

The Mil Mi-24 entered combat for the first time during the (July 1977–March 1978), when Soviet-supplied helicopters bolstered Ethiopian defenses against Somalia's invasion of the region. The , shifting alliance from to in late 1977, orchestrated a massive delivering over 1,000 aircraft, including dozens of Mi-24s, alongside military advisors and expeditionary forces. These early Mi-24A variants, characterized by their short stub wings and nose-mounted turrets, were primarily operated by Cuban pilots due to Ethiopian crews' limited training. Employed in close air support roles, the Mi-24s conducted armed reconnaissance, runs with machine guns and rockets, and escorted troop transports amid harsh desert terrain and high temperatures that challenged engine performance. Their heavy armor and firepower proved effective against Somali ground forces, including T-55 tanks and infantry, contributing to Ethiopia's counteroffensive that recaptured key towns like by January 1978. Soviet records indicate the helicopters inflicted significant casualties, with one operation alone destroying over 20 Somali vehicles, though exact loss figures for Mi-24s remain sparse, suggesting minimal attrition from Somali small arms and anti-aircraft fire. This debut validated the Mi-24's design as a hybrid gunship-transport, enabling rapid insertion of Derg-aligned militias while suppressing enemy positions, though logistical strains from dust ingestion and maintenance demands highlighted early operational limitations in prolonged hot-weather campaigns. By war's end, the Mi-24's success influenced Soviet tactics for future exports, demonstrating its utility in proxy conflicts without direct involvement. No other confirmed Mi-24 combat deployments occurred in the , with subsequent uses emerging in the .

Soviet-Afghan War (1979–1989)

The Mil Mi-24 entered combat in Afghanistan shortly after the Soviet invasion on December 27, 1979, serving as a primary gunship for close air support, reconnaissance, and strikes against Mujahideen positions. It escorted Mi-8 troop transports during insertions of special forces and conducted independent attacks on insurgent concentrations, leveraging its armament of rockets, machine guns, and bombs to suppress resistance in mountainous terrain. Early operations demonstrated high effectiveness, with Mi-24 formations disrupting Mujahideen ambushes on convoys and enabling ground advances by delivering suppressive fire from standoff ranges. Soviet tactics emphasized low-level flights to evade and maximize accuracy, but Afghanistan's high altitudes—often exceeding 2,000 meters—and thin air degraded engine performance, limiting to roughly half the sea-level capacity and restricting troop transport to minimal squads under optimal conditions. The helicopter's armored cockpit and troop compartment provided resilience against small-arms fire, allowing it to operate in contested valleys where struggled, though dust from rotors often impaired visibility and maintenance. dubbed it "Satan's Chariot" for its terrorizing impact, as rapid rocket barrages could scatter fighters and destroy fortifications before they regrouped. Losses accumulated from ground fire, with targeting vulnerable rotors using rifles and heavy machine guns like the , downing aircraft during predictable approach patterns. By mid-decade, over 300 Soviet helicopters had been lost overall, a significant portion being Mi-24 variants, due to these tactics and environmental factors. The introduction of U.S.-supplied missiles to insurgents in September 1986 escalated attrition, with portable infrared-guided systems exploiting the Mi-24's exhaust plumes; post-1986, Soviet rotary-wing losses surged, contributing to tactical shifts toward higher-altitude operations and reduced helicopter reliance. Approximately 120 Mi-24s were destroyed by war's end in 1989, underscoring vulnerabilities despite iterative modifications like infrared suppressors and enhanced armor. Despite these challenges, the Mi-24 flew thousands of sorties, supporting major offensives such as the campaigns in 1980–1984, where it neutralized strongholds through coordinated strikes with Su-25 jets. Its multi-role design allowed simultaneous troop delivery and fire support in assault operations, though high operational tempo—often 100+ hours monthly per —strained amid ambushes on forward bases. By withdrawal in February 1989, the platform's adaptability had inflicted disproportionate casualties on lightly armed guerrillas, yet its losses highlighted the limitations of airpower against dispersed, terrain-exploiting foes.

Cold War Export Conflicts (1980s)

Export variants of the Mil Mi-24, primarily the Mi-25, equipped several Soviet client states during the 1980s, enabling their use in proxy conflicts that exemplified tensions without direct superpower engagement. These helicopters provided , troop insertion, and anti-armor capabilities in environments. In the Iran-Iraq War (1980–1988), the Iraqi Army Air Corps deployed Mi-25s extensively for ground attack missions against Iranian positions, contributing to significant casualties among and armored units. Instances of air-to-air combat occurred, with Iraqi Mi-25s engaging Iranian AH-1J SeaCobra helicopters, marking rare helicopter-versus-helicopter battles. Nicaragua's Sandinista regime received 12 Mi-25s in the mid-1980s from Soviet deliveries, deploying them starting in 1985 against Contra insurgents in operations that included strikes on rebel positions. U.S.-backed reported downing at least one Mi-25 in combat on April 10, 1987, highlighting vulnerabilities to man-portable air-defense systems. Libya employed Mi-25s in its intervention in Chad's (1983–1987), supporting ground advances until defeats led to abandonments; in April 1987, Chadian forces captured two intact Mi-25s near Ouadi el Hadjar, which U.S. recovered via to analyze Soviet technology. Cuba, having acquired Mi-24s in early 1982, integrated them into its expeditionary forces in Angola's civil war, where they bolstered MPLA offensives against UNITA rebels and South African incursions through the decade.

Post-Cold War Engagements (1990s–2000s)

In the First Chechen War (1994–1996), Russian forces deployed Mi-24 helicopters for close air support and reconnaissance amid urban and mountainous fighting, but their operations were hampered by poor weather, limited intelligence, and Chechen use of man-portable air-defense systems (MANPADS) and small arms, leading to at least three Mi-24 losses in the initial three months alongside two Mi-8 transports. Overall helicopter losses remained relatively low due to cautious employment and reliance on fixed-wing aircraft like the Su-25 for most strikes, though the Mi-24's heavy armor proved resilient against ground fire in several engagements. Effectiveness was further reduced by the dispersed nature of Chechen fighters in rugged terrain, where pinpoint targeting proved challenging without advanced sensors. During the Second Chechen War (1999–2009), Russian Mi-24 variants saw expanded use starting with the 1999 invasion of and the assault on , providing troop insertion, suppression of rebel positions, and escort for convoys, with tactics evolved from the first war emphasizing standoff rocket launches and integration with to minimize exposure to anti-air threats. Approximately 20–30 Mi-24s were committed in the early phases, contributing to the rapid recapture of key areas, though Chechen forces continued to inflict losses via ambushes and Igla MANPADS, with verified shootdowns numbering around five by 2002. Russian reports highlighted improved survivability through low-altitude night operations and electronic countermeasures, but persistent vulnerabilities in urban environments underscored the platform's limitations against adaptive insurgents. Export operators also employed the Mi-24 in post-Cold War conflicts. In Angola's (resuming intensely in the 1990s until 2002), government Mi-24s flown by Angolan and mercenary pilots conducted strikes against strongholds, destroying armored vehicles and supply lines during offensives like Operation Iron Fist in 1999, though maintenance issues and UNITA's anti-tank teams downed several units. In the Eritrean-Ethiopian War (1998–2000), Ethiopian Mi-24s proved highly effective in anti-armor roles, claiming over 50 Eritrean tanks and APCs with Shturm missiles in battles around and Zalambessa, leveraging the helicopter's speed and firepower to blunt mechanized advances despite operating at high altitudes. Russian Mi-24s supported Tajik government forces against Islamist rebels in the Tajik Civil War (1992–1997), conducting raids along the Afghan border to interdict infiltrations, with minimal reported losses due to the conflict's low intensity.

Contemporary Operations (2010s–Present)

deployed Mi-24 helicopters to in late as part of their intervention supporting the Assad regime, employing them for low-altitude missions against opposition forces. These operations involved flying near ground level to evade detection and deliver and attacks on positions. Syrian government forces also relied on Mi-24 and Mi-25 variants for bombing runs, with one analysis documenting 564 bomb drops by Mi-25s between late and mid-2016 in rebel-held areas. In December 2024, Hay'at Tahrir al-Sham rebels captured and operated Syrian Mi-24s against government remnants in coastal regions following major advances. The Afghan Air Force maintained a small fleet of Mi-35 attack helicopters—export variants of the Mi-24—for counter- operations through the , participating in missions such as the July 2010 rescue of in a contested gorge. By 2015, only about two of six Mi-35s with viable service life remained operational due to maintenance challenges and high attrition. The 2021 Taliban takeover resulted in the capture of several Mi-24s, though their integration into Taliban forces has been limited, with primary focus shifting to fixed-wing assets by late 2021. In the Donbas conflict starting 2014, Ukrainian Mi-24s conducted attack sorties, with one shot down over in August 2014 by ground fire. During the full-scale Russian invasion from February 2022, continued deploying Mi-24s for strikes, including a March 2022 cross-border operation into targeting Russian fuel depots. supplied eight additional Mi-24s to from 2022 to March 2024 to bolster capabilities amid heavy losses. Russian forces have lost numerous Mi-24s to Ukrainian air defenses, exemplified by a recovery operation in September 2025 salvaging one from the submerged since April 2024. Amid the 2020 Nagorno-Karabakh war, Azerbaijani forces inadvertently downed a Russian Mi-24 on November 9, 2020, via while it escorted a convoy near the border, killing two crew and injuring one; Azerbaijan attributed it to misidentification outside active zones.

Variants

Core Soviet and Russian Models

The Mi-24A, designated Hind-A by , was the initial serial production variant of the Mil Mi-24 , entering production in 1972 and operational service with the Soviet Air Force in 1973–1974. It accommodated two crew members in side-by-side seating, eight troops, and featured armament comprising four 57 mm rocket pods, four 9M17 Falanga anti-tank guided missiles (ATGMs), unguided bombs, and a chin-mounted 12.7 mm . Approximately 240–250 units were manufactured, though early models suffered from issues including lateral roll tendencies, limited pilot visibility, and inadequate sighting systems. The Mi-24D (Hind-D), an interim evolution, initiated design work in 1971 and entered production at and Rostov plants in 1973, with service introduction around 1976. Key enhancements included a tandem arrangement for superior forward visibility, a redesigned narrower reducing frontal profile, armored glass cockpits, dust protectors on , and infrared-suppressing exhaust deflectors. Armament comprised a retractable chin turret with a 12.7 mm (1,470 rounds), up to 1,500 kg of external stores including 57 mm rockets, 500 kg bombs, and improved 9M17P Falanga-P ATGMs. About 350–550 units were built through 1977, forming the basis for subsequent upgrades. The Mi-24V (Hind-E), a major refinement of the Mi-24D, began deliveries on 29 March 1976 and remained in production until 1986. It incorporated engines for enhanced power, the SHTURM-V (9M114 Shturm) ATGM system with laser beam-riding guidance for improved accuracy and range, head-up displays, and secondary flight controls. Weapon options expanded to 80 mm S-8 rockets, GSh-23L twin 23 mm cannons, and optional air-to-air missiles like the R-60 (AA-8 ). Over 1,000 units were produced, achieving high combat effectiveness with reported kill ratios exceeding 90% in engagements. The Mi-24P (Hind-F), optimized for heavy roles, commenced development in 1974, entered service in 1982, and produced through 1990. It replaced the chin turret with a fixed side-mounted GSh-30-2 30 mm (250–260 rounds) for greater firepower against armored targets, while retaining compatibility with Shturm ATGMs, rockets, and bombs. Empty weight stood at 8,200 kg, with of 12,000 kg. Approximately 620 units were built. Post-Soviet Russian upgrades include the Mi-24VM, a modernization of Mi-24V airframes with advanced , survivability enhancements, and compatibility with modern sensors and weapons. The Mi-35M, entering production in 2005, represents a deep upgrade primarily derived from the Mi-24V, featuring non-retractable , uprated VK-2500 engines, a new rotor system for improved maneuverability, integrated electro-optical/ targeting, and provisions for precision-guided munitions like the Hermes or Vikhr ATGMs. It supports round-the-clock operations and maintains troop transport capacity, with ongoing production for Russian forces emphasizing armored target destruction.

Export and Licensed Variants

The Mi-25 designation applies to export variants of the Mi-24D, incorporating the tandem cockpit configuration with a lowered forward position for improved visibility and handling, along with enhanced navigation systems tailored for international operators. These models retained the core anti-tank and close air support capabilities of the baseline Mi-24D but featured simplified avionics in some deliveries to align with recipient nations' maintenance capacities. The Mi-35 serves as the export equivalent of the Mi-24V, equipped with TV3-117VMA turboshaft engines providing greater power and reliability, a four-bladed all-metal main rotor for improved lift, and compatibility with 9M114 Shturm (AT-6 Spiral) wire-guided anti-tank missiles launched via the Raduga-Kh system. This variant emphasized versatility in troop transport and roles, with provisions for up to 1500 kg of external ordnance including pods and free-fall bombs. Subsequent export developments include the Mi-35M, a heavily modernized iteration produced by since the early 2000s, featuring engines for enhanced hot-and-high performance, a new modular armored resistant to 12.7 mm rounds, composite rotor blades with swept tips, and an integrated mast-mounted sight for in all weather conditions. The Mi-35M incorporates digital fire control systems compatible with newer munitions like the missiles and 23 mm GSh-23L chin turret, extending operational range to approximately 460 km and service ceiling to 5,500 m. Other specialized export models, such as the Mi-35P with suppressors and night-vision equipment, address low-light operations for specific clients. Licensed production of Mi-24 derivatives outside has not been documented on a significant scale, with all major variants manufactured at the facility in and supplied directly to over 50 nations through arms export agreements. This centralized approach ensured quality control over the helicopter's complex rotor and transmission systems, which require specialized Soviet/ and assembly techniques.

Operators

Active Operators

The Mil Mi-24 series remains in widespread active service across more than 50 countries as of 2025, serving primarily in attack, , and troop transport roles, with maintaining the largest fleet. These helicopters continue to see combat use in various conflicts, including adaptations for modern threats like drones.
CountryEstimated Fleet SizePrimary VariantsNotes
Russia137Mi-24V/PLargest operator; integrated into army aviation for ongoing operations. Additional estimates suggest over 300 total across branches.
UkraineUnknown (operational)Mi-24VActively deployed in the Russo-Ukrainian War; modified with Western armaments like Hydra rockets and used for low-level strikes and drone interception.
India15Mi-24/35Operated by the Indian Air Force alongside AH-64 Apaches for attack missions.
Azerbaijan47Mi-24In service with the Azerbaijani Air Force.
Armenia20Mi-24Active in the Armenian Air Force.
Belarus25Mi-24Operated by Belarusian forces.
Hungary8Mi-24Limited active fleet in the Hungarian Defence Forces.
Additional active operators include , , , , , and , among others, where the Mi-24 supports counter-insurgency and conventional operations, though precise current fleet sizes for these nations are not publicly detailed in available sources.

Discontinued Operators

The Mil Mi-24 has been retired from service by several nations, often due to aging airframes, high sustainment costs, shortages of parts following the Soviet Union's dissolution, or transitions to Western equipment. Croatia acquired approximately 10 Mi-24D and Mi-24V helicopters from in the early 1990s amid the , employing them in roles during conflicts including in 1995. The fleet suffered losses, with at least one downed by ground fire and another crashing due to weather. All surviving units were withdrawn in 2004–2005 owing to prohibitive modernization expenses and logistical challenges. The Czech Republic's Air Force operated around 25 Mi-24V helicopters since the , accumulating over 45 years of service without deployment in foreign missions. The type was fully retired by the end of 2023 to enable procurement of and UH-1Y helicopters, with several Mi-24s transferred to for continued use in its ongoing conflict. Following in 1990, the unified inherited about 20 Mi-24D and Mi-24P helicopters from the East German . These were systematically decommissioned by 1993 as part of broader efforts to eliminate Warsaw Pact-era assets, with airframes either scrapped, donated, or preserved for display; examples include those at the in the United States.

Specifications

General Characteristics

The Mil Mi-24, known by the NATO reporting name Hind, is a twin-engine attack helicopter with combined gunship and troop transport capabilities, featuring a heavily armored fuselage designed to protect against small-arms fire up to 12.7 mm caliber and a five-blade main rotor system. It accommodates a crew of two—pilot and weapons systems officer—in tandem cockpits, with provision for an optional flight engineer, and can carry up to eight troops or equivalent cargo in its internal compartment measuring approximately 2.5 m long, 1.5 m wide, and 1.2 m high. Key dimensions include a main diameter of 17.3 m, of 3.9 m, length of 17.5 m (overall length 21.6 m with rotors turning), and height of 6.5 m with extended. The helicopter's empty weight is around 8,500 kg, with a normal takeoff weight of 11,100 kg and maximum gross weight of 11,500 kg.
ParameterSpecification
Powerplant2 × Isotov (Klimov) TV3-117 engines, 1,640 kW (2,200 shp) each
Maximum speed335 km/h (208 mph)
Cruising speed295 km/h (183 mph)
Range (normal load)450 km (280 mi)
Ferry range (with aux fuel)950 km (590 mi)
Service ceiling4,500 m (14,800 ft)
Rate of climb15 m/s (2,950 ft/min)
Hover ceiling (OGE)1,500 m (4,900 ft)
Hover ceiling (IGE)2,200 m (7,200 ft)
The Mi-24's stub wings provide lift to offload the main rotor during forward flight, enhancing speed and maneuverability, while its tricycle is retractable for improved . Internal capacity is 1,840 liters, supplemented by optional auxiliary tanks for extended operations. These characteristics enable the Mi-24 to perform in diverse roles, from armored vehicle destruction to insertion under , though its size and signature make it vulnerable to advanced air defenses.

Armament and Equipment

The Mil Mi-24 attack helicopter's primary fixed armament consists of a chin-mounted automatic gun, varying by variant and production series. Early Mi-24A models featured a four-barreled 12.7 mm Yak-B machine gun with 1,470 rounds, while later series from the Mi-24V onward typically mounted a twin-barreled 23 mm GSh-23L cannon in a retractable NPPU-23-02 turret, carrying 450 rounds. The Mi-24P variant replaces this with a fixed side-mounted GSh-30K 30 mm autocannon on the right fuselage side, firing 30x165 mm rounds at up to 1,800 rounds per minute with 250-470 rounds stored. Suspended ordnance is carried on four to six underwing pylons, supporting a maximum external weapons load of 1,500 kg. Common configurations include anti-tank guided missiles such as up to eight 9M114 Shturm (AT-2 Swatter) or (AT-9 Spiral-2) beam-riding missiles with ranges of 5-8 km; unguided rocket pods like B-8V20 with 20x 80 mm S-8 rockets or UB-32-57 with 32x 57 mm S-5 rockets; free-fall bombs including 100-250 kg FAB series or ZAB incendiaries; and occasionally 23 mm gun pods or cluster dispensers like . Air-to-air missiles such as Igla (9K38) have been integrated on some upgraded models for . Avionics and equipment emphasize targeting and , with standard electro-optical systems like the GOES-342 gyro-stabilized sight for the gunner providing day/night acquisition via TV and FLIR channels on later variants. relies on radio-inertial setups with for ground speed, while some export and modernized Mi-24s incorporate and glass cockpits. Defensive equipment includes UV-26V countermeasures dispensers launching and flares—typically 32-60 rounds per system—to counter and radar-guided threats, with post-1980s upgrades adding warning receivers and, in select models, jammers like the President-S for enhanced evasion against MANPADS.

References

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