翻訳と辞書 |
Colyaer Martin3 S100 : ウィキペディア英語版 | Colyaer Martin3 S100
The Colyaer Martin3 S100 is a Spanish ultralight aircraft, designed and produced by Colyaer of Portonovo.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 36. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 132. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕 ==Design and development== The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in pusher configuration.〔〔 The aircraft is made from composites. Its span wing has an area of and flaps that can be deployed for landing and reflexed for cruise flight. The long wingspan gives the Martin3 a glide ratio of 23:1 and allows power-off soaring flights. The standard engine is the Rotax 912ULS four-stroke powerplant.〔〔
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「Colyaer Martin3 S100」の詳細全文を読む
スポンサード リンク
翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|