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The Bagalini Bagalini is an Italian homebuilt ultralight aircraft that was designed by Marino Bagalini. The aircraft is supplied in the form of plans for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 126. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The Bagalini was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . The aircraft features a strut-braced parasol wing, a single-seat open cockpit without a windshield, fixed tricycle landing gear and a single engine in pusher configuration.〔 The Bagalini's fuselage is made from wood and metal, while the wings are a wooden frame covered in doped aircraft fabric. The rear fuselage consists of two tubes, one above and one below the pusher engine. Its span wing employs a modified NACA 63-215 airfoil at the wing root transitioning to a NACA 4412 at the wing tips. The wing has an area of and is supported by "V" struts. The acceptable power range is and the standard engines used are the Rotax 377 and the Rotax 447 two-stroke powerplants.〔 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 manufacturer estimates the construction time from the supplied plans as 700 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「Bagalini Bagalini」の詳細全文を読む スポンサード リンク
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