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Chayair Sycamore : ウィキペディア英語版 | Chayair Sycamore
The Chayair Sycamore is a South African autogyro, designed and produced by Chayair of Musina. 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 178. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The Sycamore features a single main rotor, a two-seats-in-tandem open or optionally enclosed cockpit, tricycle landing gear with wheel pants and a four-cylinder, liquid and air-cooled, four-stroke, dual-ignition turbocharged Rotax 914F engine in pusher configuration. The Subaru EJ22 is optional.〔 The aircraft fuselage is made from bolted-together aluminum tubing and mounts a diameter Advanced Kinetics rotor. The tailplane features five vertical tail surfaces for improved directional stability. The enclosed Sycamore Mk 1 version has an empty weight of and a gross weight of , giving a useful load of .〔
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「Chayair Sycamore」の詳細全文を読む
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