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MSL Aero H80 : ウィキペディア英語版 | MSL Aero H80
The MSL Aero H80 is a French ultralight aircraft that was designed by Massimo Tedesco and Sebastian Lefebre and produced by MSL Aero of Limoges-Fourches.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 66. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from sheet aluminum. Its span wing has an area of and flaps. The wing is supported by V-struts and jury struts. Standard engines available are the Rotax 912UL and the Rotax 912ULS four-stroke powerplants.〔
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「MSL Aero H80」の詳細全文を読む
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