
In numbers Through the lens Video
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. |