Overview

Data on design, manufacture and status

Design authority: Kawasaki Heavy Industries Ltd.

Primary manufacturer: Kawasaki Heavy Industries Ltd.

Parent type: Kawasaki OH-1

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: TBA

Crew seating: Tandem

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Mitsubishi TS1-M-10 turbine

Engine manufacturer: Mitsubishi Heavy Industries Ltd.

Weights and Performance

Data on aircraft weight and flight characteristics

Related VFS Resources

Resources related to the OH-1 , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the OH-1 , provided by public sources across the internet.

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