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  ·  patented distributed-propulsion vortex-lift technology  
  ·  flight-tested proof-of-concept high lift and thrust efficiency  
  ·  slow manoeuvrable flight performance  
  ·  stability in turbulence  
  ·  short take-off and landing  
  ·  ongoing development of vectored thrust for VTOL application  
  ·  low carbon footprint  for projected manned applications