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The Bradley BA-200 ATAC (or Bradley ATAC BA-200) was an American homebuilt aircraft that was designed by Bradley Aerospace of Chico, California, introduced in the mid-1990s. The aircraft was intended to be supplied as a kit for amateur construction, but is likely that only one was constructed.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 347. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕 ==Design and development== The BA-200 was conceived as a follow-on design to the Bradley Aerobat. It was intended to feature two-seats-in-tandem and aerobatic capabilities that included an airframe stressed to +/-15g.〔 The aircraft was made from all-metal construction. Its span wing had a wing area of . The cabin width was . The acceptable power range was and the standard engine used was the Volkswagen air-cooled engine .〔 The aircraft had a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passenger and baggage was .〔 The standard day, sea level, no wind, take off with a engine was and the landing roll was .〔 The manufacturer estimated the construction time from the supplied kit as 200 hours.〔 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「Bradley BA-200 ATAC」の詳細全文を読む スポンサード リンク
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