NATO: Hind-D | Export: Mi-25
A Hind-D in Polish service.
Source: Cezary Piwowarski -
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635 by 1989
Hind-D (NATO reporting name)
Mi-25 (export model)
Izdeliye 246 (article index)
2 + 8 (pilot, gunner, 8 troops)
Max take-off weight
2x Klimov TV3-117 turboshaft
Five blade main rotor
17.3 m main rotor
235 m² main rotor
Optional 500 L drop tank on each hardpoint
950 km with auxiliary fuel
2 wingtips with 2 launch rails each for 9M17P Falanga-P
1x 12.7mm Yak-B minigun
1.470 rounds ready to fire
Mi-24D armament options
1x 12.7mm Yak-B gatling un as fixed gun in chin turret
2x 9M17 Fleyta anti-tank guided missile on wingtip pylons
S-5 aerial rocket in UB-32 or UB-16 rocket pods
UPK-23 gun pod with twin barrel 23mm GSh-23L autocannon.
GUV gun pod with 12.7mm Yak-B and 2x 7.62mm GShG or a single AG-30 automatic grenade launcher.
1x FAB-250 aerial bomb
1x FAB-100 aerial bomb or 4x on MDB-4 ejector rack
1x KMGU-2 dispenser
The Mi-24D is the successor to the iconic Mi-24A with is large angular "glasshouse" cockpit.
The Mi-24V is the successor to the MI-24D. The main difference is the use of the much more capable 9M114 Shturm (NATO: AT-6 Spiral) anti-tank missiles.
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