翻訳と辞書 |
Protoplane Ultra : ウィキペディア英語版 | Protoplane Ultra
The Protoplane Ultra is a French ultralight aircraft, designed and produced by Protoplane of Bagnères-de-Bigorre. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 71. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The Ultra was designed as a highly efficient aircraft, to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.〔 The aircraft is made from composites. Its span wing employs a Wortmann FX 66-17All-182/26 airfoil, has an area of and flaps that have deflections of 0°, 15° and 35° available. The standard engine provided is the Jabiru 2200 four-stroke powerplant.〔 The Ultra achieves a fuel economy of 12l/h (43 mpg) at 220 kph (137 mph).〔
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「Protoplane Ultra」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.
|
|