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Bell Sidewinder : ウィキペディア英語版 | Bell Sidewinder
The Bell Sidewinder is an American ultralight aircraft that was designed by Fred Bell. The aircraft was supplied as a kit for amateur construction.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-33 and 37. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Design and development== The Sidewinder is a copy of the Phantom X1 that was created by former Phantom Aeronautics employee Fred Bell. It was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a cable-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from bolted-together aluminum tubing, with the flying surfaces covered in Dacron sailcloth. The Sidewinder differs from the X1 in having flaps. Its span wing is cable-braced from an inverted "V" kingpost mounted on top of the wing. The landing gear has suspension on all wheels and features a steerable nosewheel, plus main wheel brakes. The pilot is accommodated on an open seat, partially enclosed by a fibreglass fairing with a windshield. The standard engine provided was the Kawasaki TA 440A snowmobile powerplant 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「Bell Sidewinder」の詳細全文を読む
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