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  2. Tweed GT-1 - Wikipedia

    en.wikipedia.org/wiki/Tweed_GT-1

    The GT-1 has the early bubble canopy in this photo. The GT-1 was built in concert with the Whigham GW-1 as both builders shared ideas and tools. The GT-1 first flew in 1960. [1] The lower part of the GT-1's nose was constructed from a drop tank, with the upper part fabricated from fiberglass that was laid up using the drop tank as a mold.

  3. List of pusher aircraft by configuration and date - Wikipedia

    en.wikipedia.org/wiki/List_of_pusher_aircraft_by...

    Kortenbach & Rauh Kora 1973 Motor glider, 2 built; Lartin Skylark 1973 Utility Prototype; PZL M-17 1973 Trainer Prototype; Edgley Optica 1979 ducted fan observation aircraft 21 built; 1980 and later ADI Condor 1981 2 seat motorglider, unk no. built; Acapella 200 1982 homebuilt, 1 built [6] Applebay Zia 1982 1 seat ultralight motorglider, 4 built

  4. Grob G 109 - Wikipedia

    en.wikipedia.org/wiki/Grob_G_109

    The aircraft then becomes a pure glider, with a best glide ratio of around 1:28. The Porsche-derived horizontally opposed air-cooled engine had the cylinder bore increase by Grob to make the engine 2.5-litre capacity and has had its Time Before Overhaul (TBO) increased by a technote to 1,600 hours after many examples run on condition reached up ...

  5. 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.

  6. Grob G102 Astir - Wikipedia

    en.wikipedia.org/wiki/Grob_G102_Astir

    The Astir CS [Club Standard] is of composite (fiberglass/resin) construction, has a large wing area, a T-tail and water ballast tanks in its wings. The large wing area gives good low-speed handling characteristics but its high-speed performance is inferior to other Standard Class gliders. In early versions, some of the fuselage frame was wood ...

  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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