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翻訳と辞書　辞書検索 [ 開発暫定版 ] スポンサード リンク Dassault Mirage G ： ウィキペディア英語版 Dassault Mirage G The Dassault Mirage G was a French two-seat twin-engined variable-geometry prototype fighter, built by Dassault Aviation in the late 1960s. The aircraft was further developed into the twin-engine Mirage G4 and G8 variants as a multi-role jet fighter capable of both interception and nuclear strike missions. Although Dassault built and flew prototypes, the entire programme was terminated in the 1970s without the aircraft entering production.〔Green 1972, p. 84.〕 ==Development== In 1964 the French defence ministry requested a development programme on variable-sweep wing aircraft for dual land and aircraft carrier use. France had participated with the Anglo-French Variable Geometry aircraft (AFVG) before abandoning their interest; later Dassault received an order for a prototype, powered by a single Pratt & Whitney/SNECMA TF-306 turbofan in October 1965.〔 The first variable-sweep aircraft from Dassault emerged as the single-engined, two-seat Mirage G fighter in 1967, essentially a swing wing version of the Mirage F2. The wings were swept at 22 degrees when fully forward and 70 degrees when fully aft and featured full-span double-slotted trailing edge flaps and two-position leading edge flaps.〔Green 1968, p. 78.〕 Flight trials were relatively successful but no production order ensued, the Mirage G programme being cancelled in 1968.〔(Dassault Aviation - Mirage G history ) www.dassault-aviation.com Retrieved: 10 April 2010〕 Flying with the Mirage G continued however until 13 January 1971 when the sole prototype was lost in an accident. 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「Dassault Mirage G」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.