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Arplast Micro'B : ウィキペディア英語版 | Arplast Micro'B
The Arplast Micro'B ((英語:Microbe)) is a French ultralight aircraft that was designed and produced by propeller manufacturer Arplast Helice. It was supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 26. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The Arplast Micro'B was designed to comply with the Fédération Aéronautique Internationale microlight rules, with a lightened version for the US FAR 103 Ultralight Vehicles category. It features a strut-braced high-wing, a single-seat enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.〔 The Micro'B is made from a combination of welded steel and carbon fibre, with the flying surfaces made from the latter material. Its span wing is supported by a single strut per side and features automatic flaps. Standard engines included the Rotax 447 two-stroke or other small lightweight motors, mounted on the main keel tube above the cockpit.〔
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「Arplast Micro'B」の詳細全文を読む
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