The Ventura 1200 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 4500NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with an integral cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The prototype's fuselage was made from composites, with its double surface Air Creation iXess wing made from aluminum tubing and covered in Dacron sailcloth. The 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, four-stroke, dual-ignition 1000NaN0 BMW R1200 motorcycle engine that was specially modified by the French engine specialty company Sodemo Moteurs. The propeller is driven via an in-house developed reduction drive.
The prototype has an empty weight of 2450NaN0 and a gross weight of 4500NaN0, giving a useful load of 2050NaN0.
