\\ Ready for take off?

MEET OUR VERTICAL TAKEOFF AND LANDING AIRCRAFT

DESIGNED TO FOLLOW CERTIFICATION SPECIFICATIONS FROM:

A MULTI-MISSION AVIATION PLATFORM

Our platform integrates electric or hybrid-electric propulsion with vertical takeoff and conventional takeoff 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 a fully equipped cockpit and pilot controls

UNMANNED CONFIGURATION

Configured for autonomous operation without a cockpit

VTOL-CAPABILITY

Vertical Takeoff and Landing

CTOL-CAPABILITY

Conventional Takeoff and Landing

FULL-ELECTRIC PROPULSION

The system is powered solely by batteries

HYBRID-ELECTRIC PROPULSION

The system is powered by a combination of batteries and a combustion generator

\\ Breaking it down

OUR AIRCRAFT IN 3 CORE ELEMENTS

Lift-and-Cruise

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Combines 8 redundant vertical lift propellers and 2 dedicated cruise propellers to ensure reliable and efficient performance throughout all flight phases
Enables a smooth transition from vertical takeoff to forward cruise without tilting the propellers

Designed for Multi-Mission Operations

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The transporter of the air - Largest cabin with high accessibility through back and side doors
Ideally suited for patient transport, military logistics, cargo delivery, and any use case demanding a highly accessible aircraft

Rear Backloading

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Large clamshell doors enabling convenient rear loading and unloading
Easy access for loading bulky cargo, medical equipment, and patient transport

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 electrical 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?

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