The Clipper was designed as a trainer for school use and complies with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. The aircraft has a maximum gross weight of 3500NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit without a cockpit fairing, tricycle landing gear and a single engine in pusher configuration.
The Clipper was developed into the longer range Raj Hamsa Voyager.
The aircraft is made from bolted-together aluminum tubing, with its double surface Raj Hamsa-made wing covered in Dacron sailcloth. Its 10.11NaN1 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 500NaN0 Rotax 503 engine or the twin cylinder, air-cooled, two-stroke, dual-ignition 650NaN0 Hirth 2706 engine.[2]
The aircraft has an empty weight of 1600NaN0 and a gross weight of 3500NaN0, giving a useful load of 1900NaN0. With full fuel of the payload is 1720NaN0.