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Raj Hamsa Voyager : ウィキペディア英語版
Raj Hamsa Voyager

The Raj Hamsa Voyager is an Indian ultralight trike, designed and produced by Raj Hamsa Ultralights since the 1990s. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 224. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The Voyager was designed as a cross country derivative of the Raj Hamsa Clipper trainer and complies with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The aircraft has a maximum gross weight of . 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 with optional wheel pants and a single engine in pusher configuration.〔
The aircraft is made from bolted-together aluminum tubing, with its double surface Raj Hamsa-made wing covered in Dacron sailcloth. Its span wing is supported by a single tube-type aerodynamically faired kingpost and uses an "A" frame weight-shift control bar. The wing is of a smaller area and faster design than the Clipper's wing and is mounted lower on a shorter mast. The landing gear has hydraulic suspension and large diameter wheels, to permit rough field operations. The powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition Rotax 503 engine or the four cylinder, air-cooled, four-stroke, dual-ignition Jabiru 2200 engine.〔
The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is .〔




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