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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: 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:
- 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: 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: Single pusher propeller (direct drive)
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Conventional runway (CTOL)
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- Battery Capacity:
- Propulsion System: Electric vertical take-off & landing (VTOL) + forward ducted-fan propulsion
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: VTOL (vertical take-off & landing)
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- Battery Capacity: 88 kWh
- Propulsion System: Direct drive propellers (fixed-pitch)
- Service Ceiling (Max Altitude): 1,500–1,800 m (≈6,000 ft)
- Takeoff / Landing Type: Vertical Takeoff and Landing (VTOL)
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- Battery Capacity:
- Propulsion System: Direct-drive fixed-pitch composite propeller (2 m diameter)
- Service Ceiling (Max Altitude): 3,000 m (≈ 9,840 ft) under motor power
- Takeoff / Landing Type: Self-launch / glider landing
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- Battery Capacity: 92 kWh
- Propulsion System: Direct-drive electric motor with tractor propeller
- Service Ceiling (Max Altitude): 14,000 ft (4,267 m)
- Takeoff / Landing Type: Conventional runway
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- Battery Capacity: 350 kW
- Propulsion System: Hybrid configuration combining a turboprop engine, turbogenerator, and distributed electric thrusters
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Conventional runway 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: 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: 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: 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: Distributed Electric Propulsion
- Service Ceiling (Max Altitude): 1,500 ft AGL
- Takeoff / Landing Type: Vertical (VTOL)
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- Battery Capacity:
- Propulsion System: Tilt-rotor / lift + cruise configuration
- Service Ceiling (Max Altitude):
- Takeoff / Landing Type: Vertical take-off & landing (VTOL)
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- Battery Capacity: 10.5 kWh (SL) or 21 kWh (SX)
- Propulsion System: Distributed electric multirotor VTOL
- Service Ceiling (Max Altitude): 200 m (656 ft)
- Takeoff / Landing Type: Vertical (VTOL)
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