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Windward Performance SparrowHawk : ウィキペディア英語版 | Windward Performance SparrowHawk
The Windward Performance SparrowHawk is an American mid-wing, single-seat glider that was designed and is produced by Windward Performance.〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 60. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X〕 ==Design and development== The SparrowHawk was designed to fit into the US FAR 103 Ultralight Vehicles category, including that category's requirement that unpowered aircraft have a maximum empty weight of . The sailplane achieves this by utilizing a structure that is predominantly made from carbon-fiber-reinforced polymer.〔 The SparrowHawk's multi-tapered, span wing employs five different airfoils and has an aspect ratio of 18.6:1. The wing features Schempp-Hirth style spoilers on the top surface. The cockpit can accommodate pilots who range in height from . The landing gear is a fixed monowheel gear with an auxiliary tail wheel. The glider is finished with a two part polyurethane paint. The aircraft can be launched by auto-tow, winch-launch, or aero-tow by both light aircraft and ultralight aircraft. Aerobatics are not recommended.〔〔 The SparrowHawk achieves a best glide ratio of 36:1 and a minimum sink rate of 119 ft/min (0.60 m/s).
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「Windward Performance SparrowHawk」の詳細全文を読む
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