
History:
The Mi-24 HIND was the first assault
transport and gunship helicopter to enter service with the Russian
Air Force. It was developed on the basis of the Mi-8's propulsion
system. Its missions include direct air support, antitank, armed
escort, and air to air combat. The HIND was used in large numbers
in the Afghanistan War, becoming the most prominent weapon of
the conflict. The Mi-24 can be compared with the AH-64 Apache,
but the HIND is also capable of transporting up to eight fully
equipped soldiers. The Russians have deployed large numbers of
HINDs in Europe and have exported the HIND to many third world
countries. Nowadays, nearly all of the older HIND A, B and C variants
have been upgraded or modified to the HIND D or E standard, which
was introduced in 1976.
It has a five-blade main rotor
which is mounted on top of the fuselage midsection. Short weapon-carrying
wings are mounted on both sides of the fuselage. Two turboshaft
engines are mounted above the fuselage midsection. The fuselage
consists of a large, oval-shaped body. The Hind D has a nose modification
with the now traditional attack cockpit in a tandem configuration,
and a chin-mounted gun-turret. Other weapons are mounted on underwing
external stores points. Each wing has three hardpoints which makes
a total of six stations. A typical mix when targeting armor formations
- besides the turret-mounted 4-barrel 12.7-mm Gatling type machinegun
- would be AT-6 ATGMs and 57-mm rockets. The aircraft can load
additional ammunition in the cargo compartment when not carrying
troops. The armored cockpits and the titanium rotor head can withstand
20-mm cannon hits. Every aircraft has an overpressurization system
for operation in contaminated environment. Because of the aircraft’s
size and weight, it is not easily maneuverable. Therefore they
usually attack in pairs or multiple pairs, and from various directions.
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Function: |
Assault helicopter; Gunship |
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Dimensions (rotor diameter/length/height
in flight): |
17.3 m / 17.5 m / 4.25 m |
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Weight: |
11,100 kg takeoff weight (11,500
kg max.) |
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Engines: |
2 x Isotov TV-3-117 turbines with
2,200 hp each |
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Cruising speed: |
295 km/h |
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Max. speed: |
335 km/h |
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Vertical climb rate: |
15 m/s |
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Payload: |
8 fully equipperd soldiers |
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Range: |
450 km |
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Ceiling: |
4500 m |
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Armor: |
only crew compartment is protected
against small arms fire |
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Crew: |
2 |
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Typical armament: |
Turret-mounted 4-barrel 12.7-mm
Gatling type machinegun; range 1,500 m; 1470 rounds |
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and up to 4 x 57 mm S-5 rocket
pods (with 32 rockets each) |
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or up to 12 x AT-2C or AT-6C
Spiral ATGMs |
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Manufacturer: |
MIL; Russia |