Mil Mi-24K


NATO: Hind-G2


Overview

Mi-24K

A Mi-24K in service with the Macedonia air force.
Source: Igor Bozinovski @ www.aeroflight.co.uk - © copyright lies with original owner

Origin
Soviet Union
Type
Scout helicopter
Entered service
Early 1980's
Status
In service
Development
1979
Developer
Soviet Union - Mil
Production
1983 - 1989
Producer
Soviet Union
Number produced
92
Designations
Hind-G2 (NATO reporting name)
Mi-24K / Korrektirovchik
Russian for "corrector"
Izdeliye 201 (article index)
Notable users
Soviet Union
Russia

Details

Facts Mi-24K
General
Origin
Soviet Union
Type
Scout helicopter
Crew
4 (pilot, gunner, 2 recon system operators)
Dimensions
Length
17.51 m fuselage
21.35 m rotors turning
Width
6.5 m wingspan
Height
6.5 m
Empty weight
9 t
Gross weight
11 t
Max take-off weight
12 t
Propulsion
Powerplant
2x Klimov TV3-117V turboshaft
2.225 shp each
Rotor setup
Five blade main rotor
Three blade tail rotor
Diameter
17.3 m main rotor
3.91 m tail rotor
Disc area
235 m² main rotor
12 m² tail rotor
Fuel
1.840 L internal
Optional 500 L drop tank on each hardpoint
Performance
Speed
335 km/h max
295 km/h cruise
Range
450 km
950 km with auxiliary fuel
Ceiling
4.5 km
Climb rate
12.5 m/s
Armament
Hardpoints
4 hardpoints, no wingtip mounts
Fixed gun
1x 12.7mm Yak-B minigun
1.470 rounds ready to fire
Self defense
Radar warning receiver
SPO-15LM Beryoza
Flares
4-6x ASO-2V-02 with 32 flares each
IR jammer
SOEP-V1A Lipa
Sensors
Optronics
Iris optical sensor
Camera system
AFA-100
Observation system
Ruta system in crew compartment, including optical systems and computer systems

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