Technical data
Type Ka-26
Function utility
Year 1970
Crew 1-2
Engines 2*325hp Vedeneyev M-14V-26
Rotor diameter 42 feet 8 inches
Speed 170km/h
Ceiling 3000m
Range 1200km
Empty Weight 4300lb
Load 900kg
Gross Weight 7165lb

Ka-26, N.I.Kamov 'Hoodlum'

This is photo (40k) of Ka-126, but Ka-26 is seen just next in background. Photo from Sergei's Aviation Page, maintained by

Small utility helicopter. Most of the fuselage is rectangular, removable box.

850 built.

Modified August 19, 1997 Back to
Main Gate