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  2. Eiri-Avion PIK-20 - Wikipedia

    en.wikipedia.org/wiki/Eiri-Avion_PIK-20

    The PIK-20 sailplane was designed at the Helsinki University of Technology by Pekka Tammi, with advice from Ilkka Rantasalo and Raimo Nurminen. The prototype first flew on 10 October 1973. [1]

  3. Schleicher AS 34Me - Wikipedia

    en.wikipedia.org/wiki/Schleicher_AS_34Me

    The AS 34Me is a single-seat, mid-wing sailplane of composite construction, with a retractable monowheel landing gear and a T-tail. [1] The design is based upon the ASW 28 , with an unflapped wing. It can be flown with an 18 m (59 ft) span and 11.9 m 2 (128 sq ft) area or a 15 m (49 ft) span and 10.5 m 2 (113 sq ft).

  4. Glider (sailplane) - Wikipedia

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

    A glider or sailplane is a type of glider aircraft used in the leisure activity and sport of gliding (also called soaring). [ 1 ] [ 2 ] This unpowered aircraft can use naturally occurring currents of rising air in the atmosphere to gain altitude.

  5. AmEagle American Eaglet - Wikipedia

    en.wikipedia.org/wiki/AmEagle_American_Eaglet

    The AmEagle American Eaglet was a highly unorthodox ultralight sailplane marketed in the U.S. for homebuilding. It was a one-seat, high-wing braced monoplane that carried an inverted V-tail on a long boom extending from a pod-like fuselage.

  6. Monnett Monerai - Wikipedia

    en.wikipedia.org/wiki/Monnett_Monerai

    The Monnett Monerai is a sailplane that was developed in the United States in the late 1970s for homebuilding. It is a conventional pod-and-boom design with a V-tail and a mid-mounted cantilever wing of constant chord. The kit assembles in approximately 600 hours. It has bonded wing skins and incorporates 90° flaps for glide path control. The ...

  7. PZL Bielsko SZD-55 - Wikipedia

    en.wikipedia.org/wiki/PZL_Bielsko_SZD-55

    With an empty weight of about 215 kg, it is the lightest of the current standard class gliders and it's known for its excellent climbing and thermalling characteristics. [2] The SZD-55 has a cambered wing-section and performs well at lower speeds, yet when full with water ballast (it can take up to 200 liters) it is also suitable for higher ...