MIL Mi-24D HIND-D. The Mi-24 attack helicopter, NATO reporting name "Hind," is a unique Soviet design concept that does not truly have a Western counterpart. It was an attempt to combine the firepower of a heavily armed and armored helicopter gunship with the troop-carrying capability of a light assault helicopter like the Bell UH-1. While.. The Mi-24 is driven by two TV3-117 engines with output of 1,638 kW each. The Mi-24A type, (NATO code HIND-A), is the first version produced in series since 1972. The Mi-24D type (NATO code HIND-D) was put in operation in 1976, and it is a largely a modified Mi-24A type version. A double-seat cockpit has been completely remodelled, the seat of.

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The new design gained worldwide attention on Sept. 21, 1978, when test pilot Gurgen Karapetyan flew a cleaned-up Mi-24A-10 at 199.13 knots (228.9 miles per hour), a helicopter speed record that stood for eight years. The Mi-24A (codenamed Hind-A by the North Atlantic Treaty Organization) entered Soviet service in 1970.. The Hind-A was quickly replaced by improved Mi-24 variants, as described below. Only about 240 Hind-As were built in all. Small numbers were exported to four Soviet client states, including Afghanistan, Algeria, Libya, and Vietnam.. _____ MIL MI-24D HIND-D: _____ main rotor diameter: 17.3 meters (56 feet 9 inches) tail rotor diameter: 3.91.