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  2. 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

  3. SZD-49 Jantar K - Wikipedia

    en.wikipedia.org/wiki/SZD-49_Jantar_K

    The SZD-49 Jantar K was a 15m Class glider designed and built in Poland ... A one-piece forward-opening canopy with integral glare-shield gave access to the cockpit ...

  4. Rolladen-Schneider LS1 - Wikipedia

    en.wikipedia.org/wiki/Rolladen-Schneider_LS1

    LS1-f - introduced the one-piece canopy, conventional tailplane, redesigned rudder and structural changes that allowed more water ballast and higher flight mass. It also has a reduced wing incidence relative to the fuselage, resulting in noticeably better high speed performance than the earlier LS1 variants.

  5. Rolladen-Schneider LS4 - Wikipedia

    en.wikipedia.org/wiki/Rolladen-Schneider_LS4

    The design of the LS4 was influenced mainly by the experience Rolladen-Schneider had gained with the LS2 and LS3 flapped gliders. Wolf Lemke returned to a double-tapered wing planform, giving it a larger area comparatively to the LS1 and LS2, and enlarged all control surfaces: the ailerons were elongated and brought further inboard and the tailplane span was increased.

  6. Schleicher Ka 3 - Wikipedia

    en.wikipedia.org/wiki/Schleicher_Ka_3

    Both have a simple, deep, sprung landing skid reaching from the nose to under the trailing edge of the wing, assisted by a tail bumper. Their cockpits are under the wing leading edge, into which the clear canopy extends. [1] The Ka 1 first flew in 1951 and ten were built; [2] the Ka 3 followed in 1954 with fifteen eventually completed. [1]

  7. 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 ...