| FANWING | |
|
Home | Technology | News | UAV | Applications | FAQ | Simulation | Pictures | Flight clips | Articles | About Us | Contact |

| · 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 |