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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 SZD-24 Foka ： ウィキペディア英語版 SZD-24 Foka The SZD-24 Foka (Seal) (''Szybowcowy Zakład Doświadczalny'' - Glider Experimental Works) was a single-seat high performance aerobatic glider designed and built in Poland in 1960. == Development == The SZD-24 Foka was designed for competition flying in the 'Standard' class as well as aerobatic flying. The design originated from a design competition within SZD which was won by the ”Delfin”, to become the SZD-24 Foka in production. The first flight, by SP-2069, took place in May 1960 at Bielsko but results were not good with poorly performing airbrakes which were unable to limit the airspeed below VNE (Velocity Never Exceed). This posed a problem as OSTIV (''Organisation Scientifique et Technique Internationale du Vol à Voile'' – International Scientific and technical organisation for gliding) rules for the Standard class in gliding competitions stipulate that speed limiting devices must limit maximum speed to VNE or below. A second prototype was quickly built, fitted with much improved air-brakes as well as improved canopy locks and an additional access panel in the rear fuselage. Adam Zientek carried out the first flight of the second prototype on 24 May 1960 which went on to take third place in the 'Standard' class at the 1960 World Gliding Championships at Köln in Germany, piloted by Adam Witek. The SZD-24 Foka prototype was much admired for its performance, elegance, aerodynamically clean lines and comfortable semi reclined flying position. The pre-production variant, called SZD-24A, introduced more refinements and the line was steadily improved up to the SZD-32 Foka 5 final production variant. 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「SZD-24 Foka」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.