| Technical data | |
|---|---|
| Function | experimental |
| Year | 1912 |
| Crew | 2 |
| Engines | 1*100hp Gnome |
| Length | 9.0m |
| Wingspan | 11.7m |
| Wing area | 25m2 |
| Empty weight | 450kg |
| Loaded weight | 730kg |
| Wing Load (kg/m2) | 29 |
| Power load (kg/hp) | 7.3 |
| Maximum Speed | 101km/h |
|
Two-seater monoplane (pilot seated behind the observer/passenger) with fuselage of circular cross-section. Front of the fuselage was partially covered by plywood. The tail section was made of four spars and numerous tiled specially shaped ribs, covered with fabric.
Wings were covered with fabric. Aircraft carried no tailfin, just a small rudder.
Presented on the 1912 Aircraft Contest, this airplane failed to win a prize. Two shortcomings plaqued the aircraft:
| Modified September 30, 1997 |
|
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