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Gyro-Kopp-Ters Twin Eagle : ウィキペディア英語版
Gyro-Kopp-Ters Twin Eagle

The Gyro-Kopp-Ters Twin Eagle is an American autogyro, designed by Bob and Arden Kopp and produced by their company, Gyro-Kopp-Ters of Lake City, Florida. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 182. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The Twin Eagle features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear with wheel pants and a four cylinder, air-cooled, four-stroke, Subaru EJ-22 automotive conversion engine in pusher configuration.〔
The aircraft mounts a diameter Dragon Wings main rotor made by Rotor Flight Dynamics, with a chord of . Standard equipment fitted includes a hydraulic pre-rotator and dual controls. The propeller used is a four bladed Powerfin composite, ground adjustable type with a diameter. The aircraft has an empty weight of and a gross weight of , giving a useful load of .〔
The company estimates the assembly time from the supplied kit as 120 hours.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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