Mi-27 Airborne command post

Mi-27 Airborne command post. First flight: 1986
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Variant of the Mi-26 serves as an air traffic control center. It was developed in the 80's. Only two helicopters were built in total, one of which is on display at the Kharkiv Aviation University.

 


Technical specifications

DESIGNER OKB Mil
COUNTRY Russia
TYPE
Airborne command post
CREW
POWER-PLANT Two turboshaft engines Progress D-136
Power, h.p. 2x11.393
DIMENSIONS  
Length, m 33,73
Main rotor diameter, m 32,00
Tail rotor diameter, m 7,61
Height, m 8,15
WEIGHT  
Maximum take-off, kg 49.600
Normal take-off, kg -
Empty, kg 28.000
Internal fuel, l -
Warload, kg -
Payload, kg -
PERFORMANCE  
Maximum speed, km/h 295
Cruising speed, km/h 255
Range, km 800
Ferry range, km -
Combat range, km -
Service ceiling, m 4.600
Static ceiling, m 1.800
Rate of climb, m/s -
Maximum overload, g -
ARMAMENT Doesn't have (defensive).