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Aeroprakt A-36 Vulcan : ウィキペディア英語版 | Aeroprakt A-36 Vulcan
The Aeroprakt A-36 Vulcan is a Ukrainian light aircraft, designed and produced by Aeroprakt of Kiev. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 154. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The A-36 is a development of the Aeroprakt A-26 Vulcan. The design goals for the A-36 include operations over hostile terrain, the ability to take-off and land with only one engine running and the ability to operate from short runways. The resulting design features a strut-braced high-wing, T-tail, a two-seats-in-side-by-side configuration enclosed cockpit, fixed conventional landing gear with wheel pants and twin engines in pusher configuration.〔 The aircraft is of mixed construction, with the forward fuselage made from fibreglass and the tail cone from aluminum sheet. The wings and tail are aluminum, while the main landing gear legs, engine cowlings and fairings are fibreglass. Its span wing has an area of and mounts flaps. The standard engines used are the Rotax 912S four-stroke powerplant.〔 The A-36 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「Aeroprakt A-36 Vulcan」の詳細全文を読む
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