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Aviasouz Cruise
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Aviasouz Cruise : ウィキペディア英語版
Aviasouz Cruise

The Aviasouz Cruise is a Russian ultralight trike, designed and produced by Aviasouz of Kazan. 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 205. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 96. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕
The company was formed by former employees of the Tupolev Design Bureau.〔
==Design and development==
The aircraft was designed to comply 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-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 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 Rotax 582 engine, with the four cylinder, air and liquid-cooled, four-stroke, dual-ignition Rotax 912 engine optional. The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is .〔〔




抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Aviasouz Cruise」の詳細全文を読む



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