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General Electric J97 : ウィキペディア英語版 | General Electric J97 __NOTOC__
The General Electric J97 is a single-shaft turbojet engine designed and built by General Electric as a compact high-performance engine for light attack fighters and eventually a number of drone projects. ==Development and design== The J97 was based on GE's General Electric GE1/J1 series of turbojets and the engine development was financed by the United States Air Force. The original application was to be the Northrop P-530 (which later evolved into the YF-17), but it was ultimately only used in several small drone aircraft.〔J97 (1970). ''Flight International''. 1 Jan 1970.〕
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「General Electric J97」の詳細全文を読む
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