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McCulloch TSIR-5190 : ウィキペディア英語版 | McCulloch TSIR-5190
The TSIR-5190 is a five cylinder two-stroke radial piston aircraft engine developed for aircraft applications by McCulloch Motors Corporation. Joe Crover and his father patented new technologies to complete development of the engine for production use. A pair of TRAD-4180s four cylinder diesels and a single TSIR-5190 from the Western Museum of Flight are in use for development. ==Specifications (TSIR-5190)==
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「McCulloch TSIR-5190」の詳細全文を読む
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