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Colyaer Freedom S100 : ウィキペディア英語版 | Colyaer Freedom S100
The Colyaer Freedom S100 is a Spanish amphibious ultralight and light-sport aircraft, designed and produced by Colyaer of Portonovo.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The Freedom was subject to a lengthy eleven-year development process between 1995 and 2006. It was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, retractable tricycle landing gear, wing-tip pontoons and a single engine in pusher configuration.〔 The Freedom is made entirely from carbon fibre, Kevlar and fibreglass composites. Its span wing has an area of and flaps that can be deployed for landing and reflexed for cruise flight. The long wingspan gives the Freedom a glide ratio of 20:1 and allows power-off soaring flights. The standard engine is the Rotax 912ULS four-stroke powerplant.〔
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「Colyaer Freedom S100」の詳細全文を読む
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