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UPDATES
March 2006
Presently we are at the flight testing stage.
In January of 2006 I have managed to lift off VERTICALY with the AMV 211 prototype.
The AMV 211 separated from the ground approximately six inches, but in an attempt to climb higher, the presently installed Mazda 13B rotary engine detonated, and immediately stopped running.
The aircraft smoothly settled on the ground.
During hover, the AMV 211 was very stable, and responded to the control inputs.
This test event is very encouraging, and proves the validity of my concept.
The conclusion is that in order to fly safely and to obtain the desired power level for reliable VTOL flight is to switch to a turbo shaft engine.
December 2004
Since the AMV 211 was completed last October of 2003, the aircraft has gone through some modifications:
- The engine cooling system was redesigned and rebuilt to address some occassional overheating problems.
- The landing gear and the aileron control system were modified for enhanced control and safety in the air and during the landing and take off processes.
In July of 2004 an FAA airworthiness certificate for experimental aircraft was issued.
Now the aircraft is undergoing an initial testing, making solid progress toward a complete take off, landing and hover as well.
Here are some brand new photos for you to enjoy.
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