Mi-2 Civil helicopter

Mi-2 Civil helicopter. First flight: 1961 © Konstantinos Panitsidis
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Technical specifications

DESIGNER OKB Mil
COUNTRY Russia
TYPE
Civil version
CREW 1
POWER-PLANT Two turboshaft engines Klimov GTD-350P
Power, h.p. 2x450
DIMENSIONS  
Length, m 11,40
Main rotor diameter, m 14,50
Tail rotor diameter, m 2,70
Height, m 3,75
WEIGHT  
Maximum take-off, kg 3.700
Normal take-off, kg 3.550
Empty, kg 2.402
Internal fuel, l 835
Weight of transported fuel with (2) external tanks, l 1.311
Warload, kg -
Payload, kg -
- passengers up to 10
- stretcher 4
- freight in cabin 700
- with on hook 800
PERFORMANCE  
Maximum speed, km/h 250
Cruising speed, km/h 200
Range, km 350
- with external fuel tanks 722
Ferry range, km -
Combat range, km -
Service ceiling, m 4.000
Static ceiling, m 2.000
Rate of climb, m/min 420
Maximum overload, g -
ARMAMENT Doesn't have (defensive).