The first helicopter of Kaman, using the synchrocopter (intermeshing rotor) configuration.  The aircraft was built from a car chassis and solid wood 2-blade rotors.  During flight testing of the 2-place synchrocopter with tricycle landing gear, Kaman had also begun development on the K-190.

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: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Weights and Performance

Data on aircraft weight and flight characteristics

Related VFS Resources

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Related Public Resources

Resources related to the K-125 , provided by public sources across the internet.

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