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Mi-24 Hind
The HIND’s wings provide 22% to 28% of its lift in forward flight. In a steep banking turn at slower airspeeds, the low wing can lose lift while it is maintained on the upper wing, resulting in an excessive roll. This is countered by increasing forward airspeed to increase lift on the lower wing. Because of this characteristic, and the aircraft’s size and weight, it is not easily maneuverable. Therefore they usually attack in pairs or multiple pairs, and from various directions.
The Mi-24, the first helicopter to enter service with the Russian Air Force as an assault transport and gunship, was developed on the basis of the Mi-8's propulsion system. Additional missions include direct air support, antitank, armed escort, and air to air combat. The helicopter was used extensively in the Afghanistan War, becoming the "signature" weapon of the conflict. The Mi-24 is a close counterpart to the American AH-64 Apache, but unlike this and other Western assault helicopters it is also capable of transporting up to eight troops. The Russians have deployed significant numbers of HINDs in Europe and have exported the HIND to many third world countries.
The five-blade main rotor is mounted on top of fuselage midsection, while short, stubby, weapon-carrying wings are mounted at the fuselsage midsection. Two turboshaft engines are mounted above body midsection with two round air intakes located just above the cockpit and exhaust ports on the sides of engines. The Hind A fuselage consists of a large, oval-shaped body with a glassed-in cockpit, tapering at the rear to the tail boom. The Hind D fuselage features nose modification with tandem bubble canopies, and a chin-mounted turret. The swept-back tapered tail fin features a rotor on the right on some models, with tapered flats on a boom just forward of the fin.
External stores are mounted on underwing external stores points. Each wing has three hardpoints for a total of six stations. A representative mix when targeting armor formations would be eight AT-6 ATGMs, 750x 30-mm rounds, and two 57-mm rocket pods. The aircraft can store an additional ammunition basic load in the cargo compartment in lieu of carrying troops. Armored cockpits and titanium rotor head able to withstand 20-mm cannon hits. Every aircraft has an overpressurization system for operation in a NBC environment.
VARIANTS
Nearly all of the older HIND A, B and C variants have been upgraded or modified to the HIND D or E standard.
| Technical data | |
|---|---|
| Type | Mi-24P 'Hind-F' |
| Function | attack |
| Year | 1976 |
| Crew | 3 |
| Engines | 2*2200hp Isotov TV-3-117 |
| Rotor Span | 17.30m |
| Length | 21.5m |
| Height | 3.90m |
| Disc Area | 235m2 |
| Empty Weight | 8200k g |
| Maximum Weight | 12000kg |
| Speed | 322km/h |
| Ceiling | 4570m |
| Payload | |
| Seats | 8 |
| Payload (weapons) | 1275kg |
| Armament | |
| Guns | 1*g30mm fixed 2-barrel gun in the nose |
| Rockets | 4*S-8/S-13/S-24 unguided rocket pods
4*Shturm-S radio-guided anti-tank |
