The project was intended to cover some basic necessities:
structure was built in wood (3 pieces) and could be assembled / disassembled
by 4 people in few minutes. The wings were entirely covered with plywood.
it had elevons and flaps along the trailing edge, with drag - rudders near
the wing tips and terminal velocity dive - brakes in the wing central section,
and near the root.
The fuselage had a width of 60 cm., a two wheel tandem landing gear with a skid in the front, and a rear seat 30 cm. above the front one to improve visibility of the instructor. A single instrument panel is visible from both cockpits. Provisions for an oxygen reserve of 3 hours and seat parachutes were included.
|Fuselage length||03.50 m.|
|Wing Area||19.00 m2|
|Empty weight||275 kg.|
|Maximum weight||475 kg.|
|Maximum glide speed||200 km/h|
|Landing speed||60 km/h|
|Best glide ratio||1:28.5 at 75 km/h and 22.7 kg/m2 loading|