akaflieg stuttgart fs28 avispa

: 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.

akaflieg stuttgart fs28 avispa

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