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Marenco Kopter Wikipedia link

The Kopter SH09 (formerly the Marenco Swisshelicopter SKYe SH09) is a Swiss five to eight seat. Marenco Swisshelicopter Kopter SKYe SH09

Amazing Marenco Swisshelicopter.

Marenco AG is pleased to present at this year's HAI-HELI EXPO the vision of a complete new development of a helicopter family. An innovative idea for a powerful, economical and safe helicopter. The development starts with a single engine helicopter. Based on that platform, the twin-engine helicopter is developed in a further step.

Marenco Kopter

The SH09 is a light-medium helicopter, powered by a single Honeywell HTS900 turboshaft engine. It uses a shrouded fenestron tail rotor and the main rotor features a five-bladed bearingless hub; the shrouded tail rotor has a wider diameter and a thinner chord in order to increase airflow, while design aspects such as a narrow tail boom, swept-back tips on the main rotor blades, and the shrouded tail rotor offer reduced noise. The HTS900 is rated at 1,020-shaft-horsepower, providing improved performance in hot and high conditions.

Founded 2010 

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Role Helicopter
National origin Switzerland

Manufacturer Kopter
Designer Martin Stucki

First flight 2 October 2014
Status Under development

Number built 3
Program cost S₣420 million (2018)

Unit cost: $3.5 million (2016)

Aircraft production Marenco Swisshelicopter.

Kopter current. The Kopter AW09 (formerly the Marenco Swisshelicopter SKYe SH09 and Kopter SH09) is the Leonardo Helicopter Division's five-to-eight seat, single-engine multirole helicopter which is currently under development at Kopter’s facilities. It is a clean-sheet design amongst a market sector dominated by decades-old airframe designs.


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Marenco Kopter. amazing helicopters of the future.

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The first prototype P1 first flew on 2 October 2014. P2 in February 2016, P3 during November 2018

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Aircraft production Marenco.
Marenco Swisshelicopter SKYe SH09 .


General characteristics

    • Crew: 1-2
    • Capacity: 3-7
    • Length: 10.2 m (33 ft 6 in)
    • Empty weight: 1,300 kg (2,866 lb)
    • Max takeoff weight: 2,650 kg 
    • Fuel capacity: 750 liters (198 US gallons)
  • Powerplants

      • Fuel capacity: 750 liters (198 US gallons)
      • Rotor systems: 5 blades on bearingless main rotor, shrouded 120 cm tail rotor
      • Powerplant: 1 × Honeywell HTS900-2 turboshaft engine, 1,021 hp)
      • Main rotor diameter: 11 m (36 ft 1 in)


  • Cruise speed: 259–269 km/h (161–167 mph, 140–145 kn)
  • Never exceed speed: 280 km/h (174 mph, 151 kn)
  • Range: 800 km (500 mi, 430 nmi)
  • Sling-load: 1,497 kg (3,300 lb)

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