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Mil Mi-24




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The Mil Mi-24 is a large combat Helicopter Gunship and low-capacity troop transport operated from 1976 by the Soviet Air Force, its successors, and over thirty other nations.

Its NATO Reporting Name is ''Hind'' and variants are identified with an additional letter. The export versions, Mi-25 and '''Mi-35''', are denoted as ''Hind D'' and ''Hind E'' respectively. Soviet pilots called the aircraft 'letayushiy tank' or ''flying tank''. Another common nickname is 'Krokodil' (''Crocodile'') - due to the helicopter's camouflage and hull shape.


CHARACTERISTICS

The core of the aircraft was taken from the Mil Mi-8 (NATO reporting name "Hip H"), two top mounted Turboshaft engines driving a mid-mounted 17.3 m five-blade main Rotor and a three blade tail rotor. The engine positions give the aircraft its distinctive double air intake. Versions D and above include a characteristic tandem Cockpit with a "double bubble" canopy. Other components of the airframe came from the Mi-14 . Weapon hardpoints are provided by two short mid-mounted Wing s (which also provide Lift ), each offering three stations. The load-out mix is mission dependent; the ''Hind'' can be tasked with close air support, anti-tank operations, or aerial combat. The body is heavily armoured and the Titanium rotor blades can resist impacts from 12.7 mm rounds. The cockpit is Overpressurized to protect the crew in NBC Condition s. The craft uses a retractable Tricycle Undercarriage .



PROBLEMS

The comparatively high size and weight of the ''Hind'' limit its endurance and maneuverability. In tight banking turns it can roll alarmingly as the wings lose lift - this was noted during test-flights in 1969 but has still not been entirely eliminated. To counter this vulnerability, the Russians operate the aircraft in pairs or larger groups, with attacks carefully coordinated to strike from multiple directions simultaneously.

Another weakness was the possibility of the main rotor striking the tail-boom during violent maneuvers. Its high loaded weight can also limit its effectiveness as a helicopter; some reports state that with a full load the ''Hind'' needs a rolling take-off and also cannot hover. The problems with the dual-role ''Hind'' have prompted the development of the Mil Mi-28 and also the Kamov Ka-50 to replace it in the gunship role.

Also, the wings interfere with the aircraft's ability to Hover and take off vertically. In fact, the Hind is certified to hover for only about 200 hours during its entire lifetime, a consequence of its emphasis on forward speed.


COMBAT EXPERIENCE


  • The Ogaden War ( 1977 - 1978 )

  • The first use of the Mi-24 in combat was with the Ethiopian forces during the Ogaden War against the Somalis. 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 ''Hind'' gunships constituted a part of the 333 Helicopters Lost During Combat Operations In Afghanistan , an unknown number to ground fire. The cockpit was heavily armoured and could withstand even .50 cal rounds, but the ''Hind''s tail is extremely vulnerable due to the lack of armour in that section.

The heat-seeking nature of the anti-aircraft weapons employed by the Mujahideen combined with the ''Hind''s exhaust being directly under the main rotor caused the aircraft to disintegrate if hit. This was remedied later by countermeasure flares and a missile warning system being installed into all Soviet Mi-4 , Mi-8 , and Mi-24 helicopters giving the pilot a chance to evade the missile or crash-land.

During this conflict, the ''Hind'' proved effective and very reliable, earning the respect of both Soviet pilots and the Mujahideen, who scattered as quickly as possible when Soviet target designation flares were lit nearby. The Mujahideen nicknamed the Mi-24 as the "Devil's Chariot" due to its notorious reputation. One Afghan rebel said "We do not fear the Soviets. We fear their helicopters."

  • Iran-Iraq War ( 1980 - 1988 )

  • The ''Hind'' saw considerable use by the Iraqi Army during the long war with their neighbour, Iran . Its heavy armament was a key factor in causing severe damage to Iran ian ground forces. This war saw the only confirmed air-to-air helicopter battles in history with the Iraqi ''Hind''s flying against Iranian AH-1J SeaCobra s (supplied by the US military) on several separate occasions. These rare battles saw Iraq emerge with a slight edge with ten AH-1Js downed by ''Hind''s compared to six ''Hind''s downed by AH-1Js.




  • Sri Lanka 1980s

  • Sri Lanka's air force used ''Hinds'' 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 Groups . It is believed that Indian losses were considerably reduced due to the heavy fire support provided by their ''Hind'' gunships.


  • Gulf War ( 1991 )

  • The ''Hind'' was again employed heavily by Iraqis during their invasion of Kuwait , although most were withdrawn by Saddam Hussein when it became apparent that he would need them to retain his grip on power in the aftermath of the war.


  • Croatia ( 1990s - 1995s )

  • First shown in 1993, they were used in operation Storm in 1995


  • Chechnya ( 1990s - 2000s )

  • During both wars in the Russian republic of Chechnya , beginning in 1994 and 1999 respectively, Mi-24s were employed by the Russian armed forces. As with Afghanistan, however, the Mi-24s were vulnerable to rebel tactics. Dozens are believed to have been shot down or crashed during military operations. A contributing cause to these crashes is the poor Maintenance given to these aging helicopters.


  • Sudan ( 1995 - Till Date )

  • The Sudanese air force acquired six Mi-24's in 1995 which were used in Southern Sudan and the Nuba Mountains to engage the SPLA . At least two aircraft were lost within the first year of operation while not in combat, but may have been replaced.


A further twelve were bought in . Mi-24's were also deployed to Darfur in 2004 - 2005 .

  • Congo ( 2003 - Till Date )

  • This UN peace keeping mission employed the MI-25/35 helicopters from the Indian Air Force to give support to the mission. The IAF has been operating the region since 2003.


  • Macedonia ( February 2001 - August 2001 )

  • The Macedonian armed forces used the Mi-24V effectively against Albanian rebels. The Mi-24V was the most effective weapon against the terrorists, with enemy casualties mounting in their hundreds in the Aracinovo and Radusa offensives.





VARIANTS



Initially modelled on the Bell AH-1 Cobra and borrowing extensively from existing models the ''Hind'' went from drawing board in 1968 to first test-flights in less than eighteen months. First models were delivered to the armed forces for evaluation in 1970 . The Mi-24A (''Hind-B'') did have a number of problems - lateral roll, weapon sighting problems, and limited field of view for the pilot. A heavy redesign of the aircraft front section solved some of these problems.
  • The first version of this helicopter, were twelve V-24 (''Hind'') prototypes and development aircraft. One such prototype was modified in 1975 as '''A-10''' for successful speed record attempts (having reached 368km/h) with wings removed and faired over and with inertia-type dampers on the main rotor head.

  • Other early versions were the Mi-24 (''Hind-A'') armed assault helicopter, which could carry eight combat troops and three crew members. It could also carry four 57-mm rocket pods on four underwing pylons, four 9M17 Falanga (AT-2 Swatter) anti-tank missiles on two underwing rails, free-fall bombs, plus one 12.7-mm machine-gun in the nose. The Mi-24 (''Hind-A'') was the first production model.

  • It was followed up by the second production model the Mi-24A (''Hind-B''). Both the Mi-24 and Mi-24A entered Soviet Air Force service in 1973 or 1974.

  • The Mi-24U (''Hind-C'') was a training version without any armament.

  • The most common variant is the Mi-24D (''Hind-D''), a purer gunship than the earlier variants, the first to include the electronics for Anti-tank Guided Missile s 9M17 Falanga ('' AT-2 Swatter ''). The Mi-24D has a redesigned forward fuselage, with two separate cockpits for the pilot and gunner. It is armed with a single 12.7-mm four-barrel machine-gun under the nose. It can carry four 57-mm rocket pods, four 9M17 Falanga (AT-2 Swatter) anti-tank missiles, plus bombs and other weapons.

  • Small numbers of Mi-24Ds were built as Mi-24DU training helicopters.

  • The Mi-25 is the export version of the Mi-24D.

  • Later development led to the Mi-24V (''Hind-E'') which was first seen in the early 1980s. It armed with newer ATGM s, like the (9M114 Kokon, '' AT-6 Spiral '') with tube launchers. Twelve of those missile are mounted on six wing pylons.

  • The Mi-35 is the export version of the Mi-24V (Hind-E).

  • The Mi-24P (''Hind-F'') gunship version, which replaced the 12.7mm machine-gun with a fixed 30-mm cannon.

  • The Mi-35P is the export version of the Mi-24P (Hind-F).

  • Other versions of Mi-24 are the Mi-24RKR (''Hind-G1'') NBC reconnaissance model, which is designed to collect radiation, biological and chemical samples. It was first seen during the 1986 Chernobyl nuclear disaster. Also known as the '''Mi-24R''', '''Mi-24RR''' and '''Mi-24RKh (Rch)'''.

  • Mi-24K (''Hind-G2'') : Army reconnaissance, artillery observation helicopter.

  • Mi-24PS : Civil police or para-military version.

  • Mi-24E : Environmental research version.

  • Mi-35U : Unarmed training verion of the Mi-35.

  • Mi-24M : Night attack version.

  • Mi-24VP : Mi-24V armed with twin 30-mm cannon in the nose turret.

  • Mi-24W : Polish designation for the Mi-24V Hind-E.


The newest variant is the 1995 Mi-24VM, with light-weight fibre main and tail rotors to improve all-round performance, updated avionics to improve night-time operation, new communications gear, shorter and lighter wings, and updated weapon systems to include support for the Ataka, Shturm and Igla-V missiles and a 23 mm main gun. Other internal changes have been made to increase the aircraft life-cycle and ease maintenance. The Mi24VM is expected to operate until 2015 .

Since 1978 around 2,000 ''Hinds'' have been manufactured, 600 for export. The U.S. Army operates a number of Hinds in Louisiana for Adversary Training .


Operators



SPECIFICATIONS (MI-24)


  plane Or Copter copter
  jet Or Prop prop
  crew 2 (pilot, co-pilot)
  length Main 57 ft 4 in
  length Alt 175 m
  span Main 56 ft 7 in
  span Alt 173 m)</li>
  area Main ft&sup2
  area Alt m&sup2
  height Main 21 ft 3 in
  height Alt 65 m
  empty Weight Main 18,740 lb
  empty Weight Alt 8,500 kg
  max Takeoff Weight Main 26 455 lb
  max Takeoff Weight Alt 12,000 kg
  capacity 8 troops or 4 stretchers
  engine (prop) Isotov TV-3
  type Of Prop turbines
  number Of Props 2
  power Main 2,200hp
  power Alt 1,600 kW
  max Speed Main 208 mph
  max Speed Alt 335 km/h
  range Main 280 miles
  range Alt 450 km
  ceiling Main 14,750 ft
  ceiling Alt 4,500 m
  climb Rate Main ft/min
  climb Rate Alt m/s



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