MIL MI-24 HIND A

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MI-24 A Nato ('HIND A') The Mi-24 went from drawing board in 1968 to first test-flights in less than eighteen months. The first models were delivered to the armed forces for evaluation in 1971. The 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 most of these problems.The core of the aircraft was derived from the Mil Mi-8 (NATO reporting name 'Hip'): two top-mounted turboshaft engines driving a mid-mounted 17.3 m five-blade main rotor and a three-blade tail rotor. The engine configuration gave the aircraft its distinctive double air intake. Original versions have an angular greenhouse-style cockpit; Model D and later have a characteristic tandem cockpit with a 'double bubble' canopy. Other airframe components came from the Mi-14 'Haze'. Two mid-mounted stub wings provide weapon hardpoints, each offering three stations, in addition to providing lift. The loadout mix is mission dependent; Mi-24s can be tasked with close air support, anti-tank operations, or aerial combat. The Mi-24 fuselage body is heavily armored and can resist impacts from 12.7 mm (0.50 in) rounds from all angles. The titanium rotor blades are also resistant to 12.7 mm rounds. The cockpit is protected by ballistic-resistant windscreens and a titanium-armored tub. The cockpit and crew compartment are overpressurized to protect the crew in NBC conditions. #Gunship #Helicopter #HIND #HIND_A #MI24 #MI24_A #MI24A #MIL #Russian