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Glassic SQ2000 : ウィキペディア英語版 | Glassic SQ2000
The Glassic SQ2000 (also written as SQ 2000 and SQ-2000) is an American homebuilt aircraft, designed and produced by Glassic Composites LLC of Sale Creek, Tennessee. When it was available the aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 167. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The SQ2000 features a cantilever mid-wing with tip rudders and a canard, a four seat enclosed cabin accessed via doors, fixed or optionally retractable tricycle landing gear and a single engine in pusher configuration.〔 The aircraft is made from composites. Its span wing has a wing area of . The cabin width is . The acceptable power range is and the standard engine used is the Lycoming IO-360 powerplant.〔 Like many canard designs, the SQ2000 has lengthy runway requirements. The standard day, sea level take-off run is , while the landing roll is .〔
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「Glassic SQ2000」の詳細全文を読む
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