A flight vehicle includes a frame, a propulsion system coupled to the frame, a first source of power coupled to the frame and configured to power the propulsion system, a traction wheel coupled to the frame and configured for tractional engagement with a ground surface during low-speed ground operation of the flight vehicle, and a second source of power coupled to the frame and configured to power to the traction wheel.
SYSTEMS AND METHODS FOR ELECTRIC-POWERED FLIGHT VEHICLES
SYSTEME UND VERFAHREN FÜR ELEKTRISCH ANGETRIEBENE LUFTFAHRZEUGE
SYSTÈMES ET PROCÉDÉS POUR VÉHICULES AÉRIENS À ALIMENTATION ÉLECTRIQUE
2025-05-07
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR ELECTRIC-POWERED FLIGHT VEHICLES
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