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CarryAir 

The eVTOL with an

excellent Payload to Range Ratio

The CarryAir UAV based on aviation standards is designed for a perfect symbiosis of range, payload and reliability. The 6 dedicated hover rotors have a wide diameter and provide thus for efficient operation while in hover mode. The aircraft has a seperate efficient propeller for a quiet operation while in fixed wing flight mode.

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The reliability is unmatched since it has a six hover rotor design for redundancy.

The aircraft structure is manufactured from aircraft certified materials, same like used for our manned airplanes. The spacious cargo hold is integrated into the wing and does not interfere with aerodynamics during flight. It is also not exposed to external environmental factors.

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CarryAir fully electric with additional Range Extender Option

  • Reduandant dual front motor for transport and flights BVLOS with a cruise speed of 70-100 km/h 

  • Payload integrated into waterproof Aircraft Structure

  • Affordable price-performance ratio

  • Empty weight: approx.11.5kg

  • Maximum Take Off Weight:  25 kg

  • One man assembly within 2 min. possible.

  • Performance Full Electric up to 200km  (with double Battery pack and lower Payload) 

  • 6 x  Propeller for hover  

  • Max gust windspeed on hover 37 km/h (20 knots) and 47 km/h (25 knots) in flight

  • DRS Ballistic parachute optional

  • LTE Link (secured)

  • Long Range Telemetrie and RC Control (FCC 20km | CE / SRRC / MIC 12km Manufacturer's information Herelink)

  • Autonomous flight BVLOS possible

  • Typical Payload 3-5kg (Cameras, Lidar, Infrared Cameras etc.)

  • 50 Liter Compartment for Payload and Battery 

  • Detachable Wings with automatic connectors and Transportbox 

  • Performance with Gasoline Range Extender 

  • Payload 6,5 kg max @ 1 kg fuel for 1 hour filght (80 km Range)

  • Payload 5 kg max @ 2,5kg fuel for a  2,5 hour flight (200km Range)

  • Payload 1kg max @ 6,5kg fuel for a 7,5 hour flight (600 km Range)

  • The calculations are based on the LiPo batteries and a gasoline Range Extender and describe possible battery configurations with calculated results in regard to airtime and maximum range with a safety margin of 20% battery capacity remaining after landing. It must be taken into account that higher wind speeds and closely successive flight maneuvers result in shorter ranges and flight times.  

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Imprint

Striekair engineering GmbH

CEO Thomas Strieker

Karlsweg 31

33335 Gütersloh

Mobile: +49 170 38 70 409


Amtsgericht Gütersloh

HRB 12574

thomas@striekair.com

Danke für's Absenden!

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