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翻訳と辞書　辞書検索 [ 開発暫定版 ] スポンサード リンク Canadian Phase I ： ウィキペディア英語版 Canadian Phase I The Canadian Phase I is a Canadian powered parachute that was designed and produced by Canadian Powered Parachutes of Vegreville, Alberta, introduced in 2000.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page D-5. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Design and development== The aircraft was designed to comply with Canadian basic ultralight rules. It features a parachute-style high wing made from rip-stop nylon, two seats in tandem accommodation, tricycle landing gear and a single Rotax 582 engine in pusher configuration.〔 The aircraft is built from bolted-together aluminium tubing. Inflight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates shock absorber-type suspension. The standard canopy supplied was the Quantum Advantage High Performance of area. This canopy provides a cruise speed of and a payload of . A larger canopy of that provides a slower cruise speed of , a slower stall speed, a higher rate of climb and a payload of was also available.〔 Factory optional equipment included a windshield, snow skis for winter operations, electric starting, a canopy-monitoring mirror and an agricultural aircraft kit.〔 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「Canadian Phase I」の詳細全文を読む スポンサード リンク 翻訳と辞書 : 翻訳のためのインターネットリソース Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.