Mi-38 Multipurpose helicopter. First flight: 2003 © Konstantinos Panitsidis

Photos from the personal collection of Konstantinos Panitsidis


 Technical specifications      Photos      Video

 

 

 

 

  

 

 


TECHNICAL SPECIFICATIONS

DESIGNER
ΟΚΒ Mil
TYPE
Multipurpose helicopter
CREW
2
POWER-PLANT
Two Pratt &Whitney, PW-127T/S
Power, h.p.
2 x 2.500
DIMENSIONS
 
Length, m
25,22
Main rotor diameter , m
21,10
Tail rotor diameter, m
3,84
Wing span, m
-
Height, m
5,56
WEIGHT
 
Empty, kg
8.300
Normal take-off, kg
14.200
Maximum take-off, kg
15.600
Internal fuel, kg
3.796
PERFORMANCE
 
Maximum speed (H=500 m), km/h
320
Cruising speed (H=500 m), km/h
285
Ferry range, km 1.550
Range, km
885
Combat range, km
325
Service ceiling (take-off 14.200 kg), m
6.000
Static ceiling (take-off 14.200 kg), m
3.100
Payload, kg up to 6.000 kg reight in cabin or 30 passengers or 7.000 kg on hook
ARMAMENT -

 


PHOTOS Mi-38