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The Pipistrel Spider is a Slovenian ultralight trike, designed and produced by Pipistrel of Ajdovščina. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 222. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==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-tandem open cockpit with an optional cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.〔 The aircraft is made from composites and steel tubing, with its double surface wing covered in Dacron sailcloth. A number of different wings can be fitted to the basic carriage, but typical is a 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 503 or the twin cylinder, liquid-cooled, two-stroke, dual-ignition Rotax 582 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 .〔 The standard day, sea level, no wind, take off and landing roll with a engine is .〔 The manufacturer estimates the construction time from the supplied kit as 150 hours.〔 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「Pipistrel Spider」の詳細全文を読む スポンサード リンク
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