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This article was automatically translated from the original Turkish version.

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AirCar
Menzil
50-80 km
Pil
Lithium-Ion
Hız
130 km/s
Şarj
30 min DC
Oturma
2 Adults
Yapısı
Carbon Fiber
Rakım (maks.)
3000 metres
Güç (maks.)
240 kWh
Yük kapasitesi
220 kg
Motorlar
8 x Electric BLDC
Boyut
160cm x 160cm x 130cm

AirCar is a prototype of an electric vertical take-off and landing (eVTOL) aircraft equipped with fully electric and autonomous flight systems. Designed to provide an alternative solution for urban and short-distance transportation, the vehicle is specifically developed to address challenges such as traffic congestion and environmental sustainability.


AirCar Image (AA))

Physical Structure and Material Technology

  • Structural Material: The AirCar fuselage is manufactured using aerospace-grade carbon fiber composite materials to reduce weight and enhance structural durability.
  • Structural Configuration: The vehicle is optimized with an aerodynamic design to minimize air resistance. The fuselage features symmetric lifting surfaces and lightweight, high-strength motor arms.


AirCar Interior (AA)

Motor and Propulsion System

  • Number of Motors: Eight electric BLDC (Brushless DC) motors.
  • Propulsion Type: Each motor is directly connected to a propeller system and controlled independently.
  • Noise Level: A motor layout and propeller geometry designed for quiet operation ensure minimal noise pollution in urban environments.
  • Power Source: Lithium-polymer or similar high-energy-density battery systems are planned for use.

Flight Characteristics

  • Take-off and Landing: Capable of vertical take-off and landing, enabling operations in small areas similar to helicopter pads.
  • Flight Modes: Compatible with manual, semi-autonomous, and fully autonomous modes. In autonomous mode, the entire flight process from take-off to landing is managed by software.
  • Stability and Control: The multi-rotor configuration ensures high stability and precise maneuverability during flight.
  • Flight Duration: Although exact figures are not specified, average urban flight durations of 15 to 25 minutes are targeted, considering the current limits of battery technology.
  • Maximum Speed: Estimated to range between 80 and 120 km/h, optimized to balance energy efficiency and safety criteria.

Safety Systems

  • Redundant Motors: In the event of a motor failure, the remaining motors automatically adjust to maintain balance.
  • Autonomous Emergency Landing: In an emergency, the software analyzes surrounding suitable landing areas and initiates a safe landing procedure.
  • Sensor Suite: Positioning and obstacle detection are achieved using LiDAR, radar, GPS, IMU (Inertial Measurement Unit), and camera-based vision systems.
  • Cabin Safety: Equipped with seat belts, impact-absorbing structural elements, and fire-resistant materials.

Cabin and User Interface

  • Capacity: Configurations for one or two passengers.
  • Entry and Exit: Automated canopy or side door system.
  • User Interface: Touchscreen flight control panel, navigation display, and AI-assisted flight assistant.
  • Communication: Continuous connection with ground stations and emergency response lines.

First Manned Flight Test

In 2024, AirCar successfully completed its first manned flight test in Türkiye. The flight test was publicly announced by the Anadolu Agency. The two-passenger prototype achieved vertical take-off, reached a specified altitude, and then executed a safe landing during the test.


AirCar Piloted Test Flight (AirCar)

The test flight was conducted at Bilişim Vadisi with the participation of expert engineers and test pilots. During the flight, the vehicle’s aerial stability, directional control, motor response times, and system reactions to emergency scenarios were evaluated. The results demonstrated that AirCar meets technical safety standards and has achieved a performance level suitable for manned flight.

Author Information

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AuthorYeşim CanDecember 8, 2025 at 10:39 AM

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Contents

  • Physical Structure and Material Technology

  • Motor and Propulsion System

  • Flight Characteristics

  • Safety Systems

  • Cabin and User Interface

  • First Manned Flight Test

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