Developed in 1948, the K-190 is a 3-place continuation of the K-125 prototype.  Equipped with a rudder on the tail fin.  Behind the pilot is a bench that is supposed to accomodate an additional two passengers [Ref 316].  The synchrocopter was commonly used for crop dusting.

Overview

Data on design, manufacture and status

Design authority: Kaman Aircraft Corporation

Primary manufacturer: Kaman Aircraft Corporation

Parent type: Kaman K-225

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Synchropter (x2)

Crew required: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming O-435-A reciprocating

Engine manufacturer: Lycoming Engines

Take-off / rated power: 142 kW (190 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1134 kg (2500 lb)

Max Range: 378 km (204 nm)

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Related Public Resources

Resources related to the K-190 , provided by public sources across the internet.

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