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Impressed by McDonnell Douglas NOTAR (no tail rotor), Kamov tested scheme on experimental Ka-26 and now propose this multirole machine for pilot and four passengers. Single main rotor with swept tips, V-tail plus upper tailplane, skid gear. Engine not selected late 1993 and jet thruster design still in research. Prelim data assume single TVO-100 engine and 700 lit fuel. Bill Gunston "The Osprey's Encyclopedia of Russian Aircraft", 2000
Technical data for Ka-118
Crew: 1,
passengers: 5,
engine: 1 x turboshaft, rated at 522kW,
main rotor diameter: 11m,
fuselage length: 10m,
height: 2.6m,
width: 2.6m,
take-off weight: 2150kg,
internal payload: 700kg,
external payload: 700kg,
max speed: 300km/h,
service ceiling: 6150m,
hovering ceiling: 3000m
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Stack trace:
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