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Pro-Composites Freedom : ウィキペディア英語版 | Pro-Composites Freedom
The Pro-Composites Freedom is an American amateur-built aircraft, under development by Pro-Composites of Buffalo Grove, Illinois. The aircraft is intended to be supplied in the form of plans for amateur construction, with some pre-formed parts made available to speed construction.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 115. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The aircraft features a cantilever low-wing, a four seat enclosed cabin accessed by doors, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.〔 The aircraft is made from pre-formed flat fiberglass and foam composite panels which are then radius bent to shape. Its span wing employs a NACA 63A-214 airfoil at the wing root, transitioning to a NACA 63A-212 airfoil at the wing tip. The wing has an area of and the cabin will be in width. The landing gear features a fully castering nosewheel and differential braking for steering. The aircraft has been designed for engines of .〔 The manufacturer markets the design as "the only composite, plans built, 4 seat aircraft that uses a conventional - non canard - platform. It can be constructed entirely from the manuals using raw materials or from pre-formed parts."〔
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「Pro-Composites Freedom」の詳細全文を読む
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