Kopter SH09 SKYe

Attribution

Attribution

First flight 02 October 2014.  The fuselage is composed completely of Carbon-Fiber.

Overview

Data on design, manufacture and status

Latest or last design authority: Kopter Group AG
Originally designed by Marenco Swisshelicopter Ltd

Latest or last primary manufacturer: Kopter Group AG
Originally manufactured by Marenco Swisshelicopter Ltd

Parent type: No type defined

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Honeywell HTS900-2 turbine

Engine manufacturer: Honeywell Aerospace

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2650 kg (5842 lb)

Max Gross Weight (airborne): 2800 kg (6173 lb)

Max Endurance: 5.0 hrs (5.0 hrs)

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Related Public Resources

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Images