|Engines||1*100hp Gnome Monosaupape|
|Wing Load (kg/m2)||38.6|
|Power load (kg/hp)||10.0|
|Climb to 500m||6min 15sec|
|Takeoff/Landing||77m / 55m|
Development of the S-9. Smaller size, weight. Traditional fuselage structure. First modification was equipped with rigid control of ailerons - steel tubes inside the wing used to move them. Trials revealed that those ailerons are not efficient enough, so ailerons were replaced by wing twist.
Side-by-side cockpit, controls only from the left seat. On the Military Aircraft Contest in 1913 aircraft took second place.
|Modified September 2, 1997||Back to|