Technical data
Type Mi-24V 'Hind-E'
Function attack
Year 1976
Crew 3
Engines 2*2200hp Isotov TV-3-117
Rotor Span 17.30m
Length 21.5m
Height 3.90m
Disc Area 235m2
Empty Weight 8200k g
Maximum Weight 12000kg
Speed 322km/h
Ceiling 4570m
Seats 8
Payload (weapons) 1275kg
Guns 1*g12.7mm 4-barrel in the nose (covering 60° arc)
Rockets 4*UV-32-57 unguided rocket pods
4*Shturm-S radio-guided anti-tank

Mi-24V, M.L.Mil 'Hind-E'

Mi-24V, photo by Paul Nann Collection;

Introduction of another modification of the Mi-24, designated Mi-24V was delayed by development of new generation Sturm-V antitank missiles (version of the ground Sturm-S system). Despite some delays, the airborn system was ready well ahead of its ground 'prototype'.

Automatic pilot's sight ASP-17V (modification of one used on Su-17 strike aircraft) was added to reduce flight stress on a crew.

The export version with 23mm cannon instead YaKB-12.7 is designated Mi-35.

At present new 'Ataka' anti-tank complex comes to replace 'Sturm' guided missiles.

Other related WEB sites:
  • Mi-24V
  • Mi-24 at Evgeni's Red Star Combat Aircraft Page;
  • Mi-14 Hind (added 8/20/97);
  • Mi-24, Mil 'Hind'

  • Modified December 10, 1997 Back to
    Main Gate