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GEN 125
The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 191 and 238-239. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The engine is a twin cylinder two-stroke, horizontally-opposed, air-cooled, , direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces at 8500 rpm. The engine weighs .〔 The engine was designed specifically for the GEN H-4 helicopter, in which four of the engines are mounted to provide redundancy.〔
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「GEN 125」の詳細全文を読む
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