|Wing Load (kg/m2)||29.0|
|Power load (kg/hp)||10.7|
Two-seat monoplane tandem, transitional to Canard. Rear wing carried no ailerons. Small rudders were located on the wingtips, while tailfin was in the middle. Foreplane (of the smaller size) served as both ailerons and elevators, were moving as a whole piece. Later this term 'slab controls' will be invented... but not the concept.
|Modified October 2, 1997||Back to |