Technical specifications 
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NATO reporting name: Hind
Mi-25 - export modification
The two-seater helicopter army combat - transport helicopter is designed and built according to a single-rotor scheme with five-bladed and three-bladed tail rotors. The helicopter is equipped with two TV3-117 turboshaft engines with a power of 2.200 hp. each.
The helicopter was created on the basis of the Mi-24D with a modified composition of on-board equipment and was intended for countries that are not part of the Warsaw Pact.
The helicopter has been operated in countries such as: Algeria, India, Iraq, Afghanistan, Angola, Cambodia, Ethiopia, Cuba, Libya, North Korea, Vietnam, Syria, Nicaragua, Peru and Yemen.
In 1985, the Pakistan Army captured two Mi-25 helicopters of the Indian Air Force. The helicopters were handed over to the Pakistan Air Force for a thorough study of the equipment of the helicopter and its performance characteristics. Another incident occurred in 1987. when the Chadian armed forces captured three Libyan Air Force Mi-25 helicopters, one of which was handed over to the US Army.
TECHNICAL SPECIFICATIONS
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DESIGNER
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OKB Mil
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TYPE
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Multipurpose assault helicopter
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CREW
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2 + 1 (available)
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POWER-PLANT
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Two turboshaft engine Klimov TV3-117
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Power, h.p.
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2 x 2.200
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DIMENSIONS
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Height, m
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21,50
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Main rotor diameter , m
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17,30
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Tail rotor diameter, m
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3,91
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Wing span, m
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6,66
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Height, m
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-
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WEIGHT
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Empty , kg
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8.340
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Normal take-off, kg
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11.100
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Maximum take-off, kg
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11.500
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Warload, kg
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up to 2.400
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PERFORMANCE
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Maximum speed, km/h
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320
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Cruising speed, km/h
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270
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Ferry range, km
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1.125
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Combat range, km
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595
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Service ceiling, m
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4.500
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Static ceiling, m
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1.300
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Payload, kg
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1.500 or up to 8 soldiers or 4 litter
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- max
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2.400
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- or with on hook
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2.000
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| ARMAMENT | 1x12,7 mm four-barrel machine-gun YakB-12,7 mm with 1.470 rounds. - in 6 hardpoints: 4 launcher UV-32-57 32U55 mm UR S-5 or 4 Anti-tank missile 9Μ17P Falanga-PV or 4 launcher UB-32A-24. Bombs 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xKMGU-2, 2xODAB-500, 2x 3B-500. |
