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Ka-226AG Multipurpose helicopter

Ka-226AG Multipurpose helicopter. First flight: 1997 © Konstantinos Panitsidis
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Technical specifications

DESIGNER OKB Kamov
COUNTRY Russia
TYPE
Multipurpose helicopter
CREW 1 - 2
POWER-PLANT Two turboshaft engines Rolls-Roys mod 250-C20R
Power, h.p. 2x460
DIMENSIONS  
Length, m 8,10
Main rotor diameter, m 13,0
Number of blades With the distinctive coaxial rotor (contra rotating blades, 2x3)
Height, m 4,15
WEIGHT  
Maximum take-off, kg 4.000
Normal take-off, kg 3.200
Empty, kg -
Internal fuel, l -
Weight of transported fuel with external tanks, l -
Warload, kg -
Payload, kg  
- passengers 1+6
- freight in cabin up to 1.200
- with on hook 1.300
PERFORMANCE  
Maximum speed, km/h 210
Cruising speed, km/h 190
Range, km 570
Combat range, km -
Ferry range, km -
Service ceiling, m 5.400
Static ceiling, m 2.100
Rate of climb, m/min 522
Maximum overload, g -
ARMAMENT Doesn't have (defensive).





Photos Ka-226AG