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Rensselaer RP-2 : ウィキペディア英語版 | Rensselaer RP-2
The Rensselaer RP-2 (for ''Rensselaer Polytechnic design 2'') is an American mid-wing, single-seat, glider that was designed by Steven J. Winckler and produced by the Rensselaer Polytechnic Institute of Troy, New York. ==Design and development== The RP-2 was the second aircraft in Rensselaer's Composite Aircraft Program and first flew in 1985.〔 The aircraft is of mixed construction, made from carbon-fiber-reinforced polymer, Kevlar and fiberglass. Its span wing employs a Boeing 80-163 airfoil and features split flaps. The aircraft weighs just empty. The landing gear consists of a conventional glider-style monowheel. The aircraft achieved a 29:1 glide ratio.〔
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「Rensselaer RP-2」の詳細全文を読む
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