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Flying Vehicles
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Flying Vehicles
Electric Flying Vehicles (EFVs) are aircraft powered by electric motors and batteries (or hybrid-electric systems) instead of traditional jet fuel or combustion engines. They are part of the next wave of advanced air mobility (AAM), aiming to make air travel cleaner, quieter, and more efficient—especially for urban and regional transport.
- Battery Capacity:
- Propulsion System: Distributed Electric Propulsion
- Service Ceiling (Max Altitude): 1,500 ft AGL
- Takeoff / Landing Type: Vertical (VTOL)
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- Battery Capacity: 2.2 kWh total (2 packs of ~1.1 kWh)
- Propulsion System: Nose-mounted folding electric propeller
- Service Ceiling (Max Altitude): 5,000 m (soaring)
- Takeoff / Landing Type: Unpowered; FES not for takeoff
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- Battery Capacity:
- Propulsion System: Distributed Electric Propulsion (DEP)
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: VTOL
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- Battery Capacity: 17 kWh
- Propulsion System: Distributed Electric Propulsion
- Service Ceiling (Max Altitude): 3,000 m (9,842 ft)
- Takeoff / Landing Type: Vertical (VTOL)
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- Battery Capacity:
- Propulsion System: Rear pusher propeller (flight) + road drivetrain
- Service Ceiling (Max Altitude): 10,000 ft
- Takeoff / Landing Type: Conventional runway
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- Battery Capacity:
- Propulsion System: Distributed electric propulsion
- Service Ceiling (Max Altitude): ~7,874 ft (2,400 m)
- Takeoff / Landing Type: VTOL & CTOL capable
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- Battery Capacity: 60 kWh
- Propulsion System: Distributed Electric Propulsion
- Service Ceiling (Max Altitude): 3,048 m (10,000 ft)
- Takeoff / Landing Type: Vertical (VTOL)
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- Battery Capacity: 820 kWh
- Propulsion System: Twin pusher electric configuration
- Service Ceiling (Max Altitude): 32,000 ft
- Takeoff / Landing Type: Conventional runway
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- Battery Capacity: ~35 kWh (modular packs)
- Propulsion System: Distributed electric propulsion (DEP) with fixed-pitch propellers
- Service Ceiling (Max Altitude): ~2,000 m (6,560 ft)
- Takeoff / Landing Type: Vertical takeoff and landing (VTOL)
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- Battery Capacity: 8 kWh
- Propulsion System: Fixed rotor configuration on tandem wings; entire airframe tilts for transition flight
- Service Ceiling (Max Altitude): 1,500 m (5,000 ft) ASL
- Takeoff / Landing Type: Vertical Takeoff & Landing (VTOL)
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- Battery Capacity: 160 kWh
- Propulsion System: Distributed Electric Propulsion (DEP), lift + cruise design
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Vertical take-off and landing (VTOL)
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- Battery Capacity: 10.5 kWh
- Propulsion System: Multi-rotor lift + rear-wheel drive
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: VTOL + trike ground operation
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- Battery Capacity: 60 kWh
- Propulsion System: Single electric motor with 3-blade composite propeller (1.63 m diameter)
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Conventional runway operation
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- Battery Capacity:
- Propulsion System: Hybrid-electric system (battery + turbine generator)
- Service Ceiling (Max Altitude): 6,500 ft
- Takeoff / Landing Type: 150 ft
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- Battery Capacity:
- Propulsion System: Lift-and-cruise
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Vertical takeoff and landing
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