Mi-24VM Multipurpose assault helicopter

Mi-24VM Multipurpose assault helicopter. First flight: 1999
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A modernized version of the Mi-24VM based on (Mi-24V / VP) with a new electronic equipment, the Ataka-V weapon system, with the possibility of suspension of air-to-air missiles of the Igla-V complex. It is also equipped with a tail rotor of the Mi-28 type and a number of modifications to the airframe.




Technical specifications

DESIGNER OKB Mil
COUNTRY Russia
TYPE
Multipurpose assault helicopter
CREW 2 + 1 (optionally)
POWER-PLANT Two turboshaft engines Klimov TV3-117V
Power, h.p. 2x2.225
DIMENSIONS  
Length, m 18,57
Main rotor diameter, m 17,30
Tail rotor diameter, m 3,84
Height, m 4,39
Wing span, m 4,77
WEIGHT  
Maximum take-off, kg 11.500
Normal take-off, kg 10.900
Empty, kg 8.050
Internal fuel, l -
Weight of transported fuel with external tanks, l -
Warload, kg up to 804
Payload, kg  
- soldier 8
- stretcher  
- freight in cabin 1.500
- with on hook 2.000
PERFORMANCE  
Maximum speed, km/h 312
Cruising speed, km/h 260
Range, km -
Ferry range, km 1.000
Combat range, km 415
Service ceiling, m 5.700
Static ceiling, m 3.000
Rate of climb, m/s -
Maximum overload, g -
ARMAMENT
One 23mm GSh-23L gun with 250 rounds. Number external hardpoints: 6. Transportation of weapons: up to 16 anti-tank missiles 9Μ120 Ataka-V, 2x9M39 Igla-V, 4xB-8V20A (S-8DM, S-8BM, S-8VM, S-8KOM, S-8S), 4xB-13L1 (S-13, S-13T, S-13-OF), 4xS-24, 2xGUV-1, 4xGUV-8700, UPK-23-250, 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xKMGU-2, 2xODAB-500, 2x3B-500.