Nine-passenger hybrid-electric fixed-wing aircraft using eight distributed electric propellers to blow high-lift wings for ultra-short runway operation; it is not a VTOL aircraft.
In development; FAA certification basis established (not type-certified)United States
Callouts below refer to the component-topology diagram, not to an unverified position on the artistic rendering.
1
Distributed blown lift
Eight small electric propellers accelerate airflow over the wing; landing and takeoff goals require validated handling margins.
2
Hybrid power generation
A compact turbine generator and energy-storage system distribute electrical power through redundant controls.
3
Short-runway design
The 150-ft requirement is an advertised objective, not proof of a certified takeoff or landing envelope.
Model identification
How to recognize this configuration
Program facts sourced · visual geometry held
01 · IDENTIFIEREight electrically driven propellers distributed along the wings.
02 · IDENTIFIERFixed-wing STOL aircraft; does not hover or perform vertical takeoff.
03 · IDENTIFIERTurbogenerator and batteries form a hybrid electric-power architecture.
The illustration is an independent editorial interpretation, not a photograph or an OEM-authorized three-view. The technical diagram preserves cited component counts while dimensions remain non-dimensional.
Detailed configuration view
An alternate-angle CGI visualization of the aircraft. Use the linked sources and specification tables for technical facts; image dimensions and component positions remain illustrative.
Source and image policy. Specifications are model-specific. All development targets are explicitly separated from certified or demonstrated measurements. Technical artwork is educational and not approved manufacturer geometry.
