. "1"^^ . . . . . . . . "2"^^ . . "48755543"^^ . . . . . . "The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty."@en . "42.5"^^ . "maximum,"@en . "11.4"^^ . "G\u00F6ttingen 387"@en . "1.7"^^ . "6.2"^^ . . "wing extensions retracted\n:::: wing extensions extended\n*Take-off speed: \n*Landing speed: wing extensions retracted\n:::: wing extensions extended"@en . "metal fixed-pitch propeller"@en . . "met"@en . . . . "355"^^ . . . . . . "7200.0"^^ . "1"^^ . . "five cylinder radial"@en . "1109638556"^^ . . "10957"^^ . . . "470"^^ . "1.9"^^ . . . . . "2930"^^ . . . . . . . . . "wing extensions retracted\n:::: wing extensions extended"@en . . . "1"^^ . "Experimental variable wing area aircraft"@en . "*Take-off distance into wind, minimum wing extension: \n*Take-off distance into wind, maximum wing extension: \n*Landing run, minimum wing extension: \n*Landing run, maximum wing extension:"@en . . "12.75"^^ . . . . . . "equipped"@en . . . . . . . . "wing extensions retracted\n:::: wing extensions extended"@en . . . "General: L'A\u00E9rophile February 1933 Performance: Flugsport March 1932, Flugzeug-Typenbuch 1944"@en . . "The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty."@en . "300"^^ . . "2"^^ . "1932-01-12"^^ . . . "1"^^ . . "wing extensions retracted\n:::: wing extensions extended"@en . . . . "Werner Schmeidler, Neumann"@en . "Schmeidler SN.2"@en . "fuel ; oil"@en . "160"^^ . . . .