Navar Falcon

Specifications:

Aircraft type

Long-range high-performance hybrid-electric VTOL passenger concept design aircraft

Piloting

1 pilot (in the future, remote or autonomous piloting)

Capacity

1 passenger and luggage (With remote or autonomous piloting, 2 passengers and their luggage)

Cruise speed

High-speed

Range

Long range

Propellers

3 advanced high-performance electric-duct-fan in wing

Electric motors

9 electric motors

Power source

Hybrid-electric power source (in the future, hydrogen fuel cells or batteries)

Fuselage

Carbon fiber composite

Window

Canopy over cockpit

Wings

1 main transformers wing with winglets

Tail

2 angled and swept forward vertical stabilizers

Landing gear

Retractable tricycle landing gear. The outer portion of the main wing folds up and then inward and part of the wing becomes the forward landing gear. The rear vertical stabilizers angle down and become the rear landing leg.

Safety features

Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.