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The 2003 AMV 211 VTOL experiment with ducted-fan propulsion. A 450hp turbocharged Mazda rotary driving a belly-mounted, 94″ five-blade prop. Wings were set at an angle to the fan, and the fuselage itself provided lift. Take-off was with the fan horizontal, blowing downward. As the ship tilted forward, wings would provide lift and the fan would then start blowing rearward through a system of louvers. For landing, the process was reversed.
Engine: 450hp turbocharged Mazda rotary
Prop: 94″ five-blade
Wingspan: 20’0″
Length: 20’0″
Useful load: 900 lb
fdr: Attila Melkuti
Aliso Viejo CA.
USA
Developed the AMV 211 in 2003
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