Mil Mi-24

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 the 'crocodile'.

Contents

1 Characteristics 2 Problems 3 Combat experience 4 Variants 5 Specifications (Hind D)

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 above the equally characteristic tandem cockpit. Other components of the airframe came from the Mi-14. Weapon hardpoints are provided by two short mid-mounted wings (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, 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 conditions. 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.

Combat experience

The aircraft was operated extensively during the Soviet invasion of Afghanistan. The US supplied Stinger missiles to the Mujaheddin, and the Hind was a favourite target. Roughly 300 were lost during combat operations in Afghanistan, an unknown number to missile hits. The cockpit was heavily armoured and could easily take .50 cal rounds, but a single lucky shot to the fuel tank could set the Mi-24 ablaze. As well, the heat-seeking nature of the FIM-92 combined with the Hind's exhaust being directly under the rotor caused the aircraft to disintegrate if hit. This was remedied later by "Hot Bricks" being put into the tail of the aircraft giving the pilot a chance to evade or crash-land. Still, the Mi-24 proved effective and very reliable, earning the respect of both Soviet pilots and Mujaheddin. The Hind also saw combat in Sri Lanka when the IAF detachment was deployed there in support of the Indian Army. It is believed that losses to the Army were considerably reduced due to the heavy fire support provided by the Hinds.

It was also used quite successfully by the Sandinista Army during the Nicaraguan civil war in the eighties.

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-A) 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 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 missiles 9M17 Falanga (AT-2 Swatter). Later development led to the Mi-24V (Hind-E) with newer ATGMs (9M114 Kokon, AT-6 Spiral) with tube launchers, and then the Mi-24P (Hind-F), which replaced the 12.7mm machinegun with a fixed 30mm gun.

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 .

Specifications (Hind D)

• Length: 17.5 m (fuselage)
• Height: 6.5 m (gear down)
• Wing span: 6.5 m
• Rotor diameter: 17.3 m
• Weight: 8,500 kg (empty), 12,000 kg (max. take-off)
• Power: Two Isotov TV-3 turbines, 2,200 shp (1.6 MW) each
• Speed: (uncertain) 335 km/h (max.), 260 km/h (cruise)
• Ceiling: 4,500 m (reported), 1,500 m (hover), spotted at over 6,000 m
• Crew: 2
• Cargo: Eight troops or four stretchers
• Armament: 12.7 mm YaKB-12,7 Yakushev-Borzov multi-barrel machinegun, four Anti-tank guided missiles and 1,500 kg of other weapons load on 4 hardpoints (typical: 4 of 57 mm rocket pods or bombs)
• Range: 450 km