Anemone is an experimental aircraft that has been manufactured recently by the project. Anemone carries a variety of sensors and electronic systems in order to gather data during flight, such as velocity, acceleration, position, altitude and pressure. This data will be crucial for the development of our next generation UAVs, so that the Aerodynamics Design and the Structural sub-system will have more information that will assist them in performance and detailed design optimization. Anemone has to achieve a certain flight time in order to collect this data.

Technical Characteristics:

  • Wingspan: 2.00 m
  • Wing Area: 0.392 m2
  • Aspect Ratio (AR): 10.20
  • Airfoil: NACA 6413
  • Length: 1.30 m
  • Powerplant: Joker 3542-5.5 V3 (940)
  • Propeller: APC Electric 9×7
  • Power: 360 W

  • Empty Weight: 2.4 kg
  • Payload: 1.2 kg
  • Take-off Weight: 3.6 Kg
  • Cruise Speed: 12 m/s
  • Stall Speed: 8 m/s
  • Maiden Flight: 25/09/2021
  • Tail configuration: T-tail

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