Mi-24A Hind Multipurpose assault helicopter

Mi-24A Hind Multipurpose assault helicopter. First flight: 1969 © Konstantinos Panitsidis
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Technical specifications

DESIGNER OKB Mil
COUNTRY Russia
TYPE
Multipurpose assault helicopter
CREW 2 + 1 (optionally)
POWER-PLANT Two turboshaft engines Klimov TV3-117
Power, h.p. 2x2.200
DIMENSIONS  
Length, m 21,50
Main rotor diameter, m 17,30
Tail rotor diameter, m 3,91
Height, m 3,90
Wing span, m 6,66
WEIGHT  
Maximum take-off, kg 11.000
Normal take-off, kg 10.500
Empty, kg 7.675
Internal fuel, l -
Weight of transported fuel with external tanks, l -
Warload, kg up to 1.275
Payload, kg  
- soldier 8
- stretcher 4
- with on hook 2.000
- freight in cabin 1.500
PERFORMANCE  
Maximum speed, km/h 320
Cruising speed, km/h 270
Range, km 450
Ferry range, km 1.000
Combat range, km -
Service ceiling, m 4.950
Static ceiling, m 1.500
Rate of climb, m/s -
Maximum overload, g -
ARMAMENT NUV-1 mobile cannon with a 12.7 mm (A-12,7) barrel, with 900 rounds.Number external hardpoints: 6. Transportation of weapons: Four 9M17M "Falanga-M" anti-tank missile, 4xUB-32A-24 (128 NAR unguided missiles - S-5M1, S5MO, S-5KBP, S-5KO or S-5-0). Bombs: 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xODAB-500, 2x3B-500, 2x pods KMGU-2.





Photos Mi-24A