Mi-24PN Multipurpose assault helicopter. First flight: 2002

 


 Technical specifications      Photos      Video

 

 

NATO reporting name: Hind
Produced: since 2003
Number built: 11-14 (all helicopters were delivered in 2004)
Export: One Ugandan Air Force helicopter

Two-seater helicopter, modernized army combat-transport helicopter of round-the-clock action (performance combat missions at night) with a new set of equipment. A modified TPP-9S475N (thermal imaging sighting system / night sighting guidance subsystem) was installed on the helicopter's.

Performance characteristics TPP-9S475N

Thermal channel spectral range, μm 8....12
Field of view of the thermal imaging channel, in deg.  
- wide field of view 7,0х11,2
- narrow field of view 2,1х3,4
Photodetector  
- ruler 128 e.
- material CMT (Cadmium-mercury telluride)
- cooling system MKS split-stirling type
Laser rangefinder wavelength, μm 1,06
Range of pointing angles of line-of-sight, deg  
- in vertical direction from -20 to +15
- by horizon from -15 to +15 (is being finalized to + 30)

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Mil
TYPE
Multipurpose assault helicopter
CREW
2 + 1 (option)
POWER-PLANT
Two turboshaft engine Klimov TV3-117V
Power, h.p.
2 x 2.225
DIMENSIONS
 
Length, m
17,51
Main rotor diameter , m 17,30
Tail rotor diameter, m
3,91
Wing span, m
4,77
Height, m
3,90
WEIGHT
 
Empty, kg
8.570
Normal take-off, kg
11.300
Maximum take-off, kg
11.500
Warload, kg
up to 2.400
PERFORMANCE
 
Maximum speed, km/h
320
Cruising speed, km/h
270
Ferry range, km
1.000
Combat range, km
450
Service ceiling, m
4.500
Static ceiling, m
2.000
Payload, kg
up to 8 soldiers or 4 litter or 1.500 kg
- max
2.400
- or with on hook
2.000
ARMAMENT 1x two-barrel 30 mm cannon GSh-30K (250 rounds). Weapon transportation: on 6 hardpoints. 16 Anti-tank missile 9Μ120 Ataka-V, 4x9M114K Shturm-V. 4xlauncher UB-32A-24 or 4xB-8V20A, 4xB-13L1, 4xS-24, 2 x GUV-1, 4xGUV-8700, UPK-23-250, 8xOFAB-100, 4xOFAB-250, 4xRBK-250, 2xRBK-500, 2xKMGU-2, 2xODAB-500, 2x3B-500.