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The Schleicher Condor, also referred to as the Dittmar Condor, is a series of German high-wing, single and two-seat, gull winged, gliders that were designed by Heini Dittmar in the 1930s, produced in small quantities before the Second World War, produced again between 1952 and 1955 by Alexander Schleicher GmbH & Co and also by Ferdinand Schmetz.〔Said, Bob: ''1983 Sailplane Directory, Soaring Magazine'', page 104, Soaring Society of America November 1983. USPS 499-920〕 ==Design and development== The first Condor I was introduced in 1932. The aircraft was further developed into the Condor II and the IIA, which replaced strut bracing with a cantilever wing. Following the Second World War the two-seat Condor IV first flew in 1951 and was put into series production by Schleicher.〔〔 The Condor series was built from wood, with the wooden-framed wing covered in doped aircraft fabric. The Condor IV has a span wing that employs a Goettingen 532 airfoil at the wing root, changing to a NACA 0012 section at the wing tip. The wings have balanced DFS-style dive brakes for glidepath control. The horizontal stabilizer is of an all-flying tail design. The landing gear was originally a dolly for take-off, with the aircraft landing on a fixed skid, although at least one was modified to use a fixed monowheel.〔〔 Some sources state that there were a total of 18 Condors constructed,〔〔 while one other says that the total number is unknown, but includes at least 18 Condor IVs built under licence in Argentina.〔VGC News no. 133, Summer 2011, Vintage Glider Club〕 At least one Condor was converted to a motorglider.〔 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「Schleicher Condor」の詳細全文を読む スポンサード リンク
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