Ka-50-2 Erdogan Multipurpose assault helicopter

Ka-50-2 Erdogan Multipurpose assault helicopter. First flight: -
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Ka-50-2 Erdogan tandem-seat combat helicopter featuring an Israeli avionics suite and designed in 1999 to compete in a Turkish armed forces-held tender for a new combat helicopter, etc.

 


Technical specifications

DESIGNER OKB Kamov
COUNTRY Russia
TYPE
Multipurpose assault helicopter
CREW 2
POWER-PLANT Two turboshaft engines Klimov TV3-117VMA
Power, h.p. 2x2.200
DIMENSIONS  
Length, m 14,50
Main rotor diameter, m 16,00
Number of blades With the distinctive coaxial rotor (contra rotating blades, 2x3)
Height, m 4,95
Wing span, m 7,34
WEIGHT  
Maximum take-off, kg 11.300
Normal take-off, kg 9.700
Empty, kg 7.692
Internal fuel, l -
Weight of transported fuel with external tanks, l -
Warload, kg 2.500
PERFORMANCE  
Maximum speed, km/h 300
Cruising speed, km/h 275
Lateral speed, km/h 100
Reverse speed, km/h 100
Range, km 1.160
Ferry range, km -
Combat range, km 450
Service ceiling, m 6.000
Static ceiling, m 4.200
Rate of climb, m/min 780
Maximum overload, g -
ARMAMENT One 20 mm cannon GIAT or one 30 mm cannon 2A42 with 480 rounds. Number external hardpoints: 6. Transportation of weapons: 12 Anti-tank missile Vihr or 16 Hellfire, 4 Air-to-air missile AIM-92 Stinger, 2 Launcher 40x80 mm or 70 mm, cannon and machine-guns pods.