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The BRM Aero Bristell is a Czech low-wing, two-seat in side-by-side configuration, single engine in tractor configuration, ultralight and light-sport aircraft that was designed by Milan Bristela and is produced by BRM Aero. The aircraft is supplied as a complete ready-to-fly aircraft. The aircraft was introduced at the AERO Friedrichshafen 2011 show.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 34. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The aircraft was designed to comply with both European microlight rules and also the US light-sport aircraft regulations, by using different versions for each regulatory environment.〔〔 The aircraft is made from aluminium and features a wide cabin at the shoulder, with a bubble canopy over the cockpit. The wings feature flaps. The standard engine is a Rotax 912UL, with the Rotax 912ULS, the ULPower UL260i/iS and the ULPower UL350iS powerplants optional. The Rotax 914, Jabiru 2200 and Jabiru 3300 are also available. Other engines are planned, particularly for the United States market. The aircraft has a notably high useful load of . The landing gear is of tricycle configuration.〔〔 After 42 examples had been completed the aircraft was introduced into the US market in September 2011 at the AOPA Summit.〔 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「BRM Aero Bristell」の詳細全文を読む スポンサード リンク
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