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  2. Schleicher Ka 6 - Wikipedia

    en.wikipedia.org/wiki/Schleicher_Ka_6

    The Schleicher Ka 6 is a single-seat glider designed by Rudolf Kaiser, [1] built by Alexander Schleicher GmbH & Co, Germany and is constructed of spruce and plywood with fabric covering. The design initially featured a conventional tailplane and elevator which was later replaced by an all-moving tailplane in the -Pe and Ka 6E variants. Variants ...

  3. Phoenix Air Phoenix - Wikipedia

    en.wikipedia.org/wiki/Phoenix_Air_Phoenix

    Data from World Directory of Leisure Aviation 2011-12 and Phoenix Air General characteristics Crew: one Capacity: one passenger Length: 6.50 m (21 ft 4 in) Wingspan: 15 m (49 ft 3 in) Height: 1.45 m (4 ft 9 in) Empty weight: 295 kg (650 lb) Gross weight: 472.5 kg (1,042 lb) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp ...

  4. Schleicher K 8 - Wikipedia

    en.wikipedia.org/wiki/Schleicher_K_8

    A motor glider conversion of the K 8B was developed by LVD (the Flying Training School of the Detmold Aero Club) similar to their conversion of a Scheibe Bergfalke IV known as the BF IV-BIMO, in which a Lloyd LS-400 piston engine mounted in the fuselage drives a pair of small two-blade pusher propellers rotating within cutouts in each wing near the trailing edge.

  5. Paragliding - Wikipedia

    en.wikipedia.org/wiki/Paragliding

    Paragliding pilots most commonly lose their height by flying a figure 8 over a landing zone until they reach the correct height, then line up into the wind and give the glider full speed. Once the correct height (about a metre above ground) is achieved the pilot will stall the glider in order to land. Landing figure 8 pattern

  6. Glider (aircraft) - Wikipedia

    en.wikipedia.org/wiki/Glider_(aircraft)

    Single-seat high performance fiberglass Glaser-Dirks DG-808 glider Aerobatic glider with tip smoke, pictured on July 2, 2005, in Lappeenranta, Finland. A glider is a fixed-wing aircraft that is supported in flight by the dynamic reaction of the air against its lifting surfaces, and whose free flight does not depend on an engine. [1]

  7. Schempp-Hirth Standard Cirrus - Wikipedia

    en.wikipedia.org/wiki/Schempp-Hirth_Standard_Cirrus

    It is a Standard Class glider with a 15-metre span, and laminar-flow airfoil section designed by Professor Franz Wortmann. The all-moving tailplane, a feature of many designs of that period due to its theoretically higher efficiency, caused less than desirable high-speed stability characteristics, and so modifications were made to the early design.

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