Kopter SH09 SKYe
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 characteristicsVTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Fenestron/Shrouded tail rotor
Crew required: 1-2 in Side-by-side arrangement
Landing gear: Skids
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentRelated VFS Resources
Resources related to the SH09 SKYe, provided by the Vertical Flight Society.Forum Proceedings
Vertiflite articles
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Web files from vtol.org
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Webpages from vtol.org
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Images from the VFS Gallery
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Related Public Resources
Resources related to the SH09 SKYe, provided by public sources across the internet.Publicly-funded resources provided by the US Government
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Public resources provided by select scholarly and academic sources
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