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
09.01.2025
Patent
Elektronische Ressource
Englisch
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