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Paraavis Sova : ウィキペディア英語版 | Paraavis Sova
The Paraavis Sova is a Russian paramotor that was designed and produced by Paraavis of Moscow for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 71. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X〕 ==Design and development== The Sova was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single Sova engine in pusher configuration with a 2.4:1 ratio reduction drive and a diameter two-bladed wooden propeller. The fuel tank capacity is .〔 As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.〔
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「Paraavis Sova」の詳細全文を読む
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