The company was formed by former employees of the Tupolev Design Bureau.
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. The aircraft has a maximum gross weight of 4300NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-side-by-side configuration open cockpit with a unique fibreglass cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with its single surface wing covered in Dacron sailcloth. Its 101NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition 640NaN0 Rotax 582 engine, with the four cylinder, air and liquid-cooled, four-stroke, dual-ignition 800NaN0 Rotax 912 engine optional. The aircraft has an empty weight of 1800NaN0 and a gross weight of 4300NaN0, giving a useful load of 2500NaN0. With full fuel of the payload is 2140NaN0.