: Two Length:.20 m (23 ft 7 in) Wingspan:.40 m (30 ft 10 in) Aspect ratio: 7 Airfoil : Eppler 530 Empty weight: 640 kg (1,411 lb) Max takeoff weight: 950 kg (2,094 lb) Fuel capacity: 115 L (25.3 I,p gal;.4 US gal) Powerplant: 1 Lycoming O-235 -E2A air-cooled flat. Wikipedia article written by contributors ( read / edit ). Credit: ( see original file ). The three blade propeller was later replaced by a two-blade one. Carmam Sa Moulins.
Flugwissenschaftliche Vereinigung Aachen. Several have designed and built aircraft, often technically advanced and leading the development of gliders in particular. 3 The sole Avispa, V-1, D-eafs, made its first flight on 20 December 1972. European registers handbook 2010.
2, the Avispa is a twin-boom, pusher configuration low mid-wing monoplane. Cover photo is available under :me 'Unknown' license. Jane's All the World's Aircraft 1974-75. Fraunhofer Society and the Ministry of Economics of Baden-Württemberg, was intended to transfer the knowledge about high performance aerodynamics and composite materials gained from glider design to light powered aircraft. 2 3 The tail booms are slender and linked at the rear by the unusual inverted Vee empennage. Images, videos and audio are available under their respective licenses. Rolladen-Schneider Flugzeugbau GmbH. Königswinter: eqip Werbung Verlag GmbH. The Avispa has a retractable tricycle undercarriage with glass fibre shock absorbers, mainwheel hydraulic brakes and a steerable nosewheel. Operational history edit keser reisen hagen The Avispa was seriously damaged in an accident in May 1981 and its permit to fly (PTF) lapsed that November.
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