\\ Ready for take off?

MEET OUR VERTICAL TAKE-OFF AND LANDING AIRCRAFT

DESIGNED TO FOLLOW CERTIFICATION SPECIFICATIONS FROM:

A MULTI-MISSION AVIATION PLATFORM

Our platform integrates electric or hybrid-electric propulsion with vertical take-off and conventional take-off capabilities. It also uses modular mission architecture to support a wide range of operational needs. All systems follow certification aligned design principles to meet requirements from EASA and FAA for performance, safety and redundancy.

MANNED CONFIGURATION

Configured with full cockpit and pilot controls.

UNMANNED CONFIGURATION

Configured without cockpit for autonomous operation.

VTOL-CAPABILITY

Vertical Take-Off and Landing

CTOL-CAPABILITY

Conventional Take-Off and Landing

FULL-ELECTRIC PROPULSION

System powered solely by batteries.

HYBRID-ELECTRIC PROPULSION

System powered by a combination of batteries and a combustion generator.

\\ Breaking it down

OUR AIRCRAFT IN 3 CORE ELEMENTS

Lift-and-Cruise

Learn more

Combines redundant 8 vertical lift propellers and 2 dedicated cruise propellers for high robustness and efficiency during all flight phases
Enables smooth transition from vertical take-off to forward cruise without tilting the propellers

Designed for Multi-Mission Operations

Learn more

Transporter of the air - Largest cabin with high accessibility through back and side doors
Highly suitable for patient transportation missions, military logistics, cargo and other use cases that require an accessible aircraft

Rear Backloading

Learn more

Large clamshell doors for rear access
Easy loading of bulky cargo, medical equipment, and patients

Our use cases

Select a topic to explore:

Design
Propulsion architecture and Flight Performance
Safety

Design
Takeoff & Landing
VTOL with CTOL capability for flexible deployment
Rotor Configuration
8 vertical propellers + 2 horizontal propellers (Lift & Cruise)
Flight Control System
Fly-by-Wire
Cabin Volume
5.2 m³
Payload Capacity
500+ kg
Clamshell Door Size
1.4 m x 1.4 m
Wing Span
15.2 m

Propulsion architecture and Flight Performance
Propulsion System
Full-Electric or Hybrid-Electric
Hybrid-Electric Range
800 km (500 mi)
Electric Range
200 km (125 mi)
Cruise Speed
220 km/h (120 knots)
Charge Time
80% of charge in 20 minutes

Safety
Certification Standard
EASA SC-VTOL first, FAA subsequently
Catastrophic Failure Rate
1 in a billion (10⁻⁹)
Propulsion Safety
Redundant electric system with backup batteries
Comparative Safety
As safe as a twin-engine helicopter (according to certification standard C29)
Ground Safety Design
Wing height of 2.2 m, with propellers positioned above the fuselage to ensure safe movement around the aircraft at all times

\\ Ready for take off?

Contact us

Tell us what you want to talk about.

Work with us
Become a partner
Press Inquiry
Investor Inquiry
Supplier inquiry