Antonov A-15

Last updated
A-15
Antonov A-15 1999 by Jiri Havlice.jpg
Antonov A-15 registered in the Czech Republic
Role Glider
National origin USSR
Manufacturer Antonov
Designer Oleg Antonov
First flight26 March 1960
Number built350

The Antonov A-15 is a Soviet mid-wing, V-tailed single-seat, FAI Open Class glider that was designed by Oleg Antonov and produced by Antonov. [1]

Contents

Design and development

The A-15 was a follow-on design, based on the bureau's experience gained with the A-11 and A-13 gliders. This new open class design quickly proved its worth as a record-setter. [1]

The aircraft is made from aluminium. Unusually for a Cold War Soviet aircraft, its 17 m (55.8 ft) span wing employs an American NACA 64-618 airfoil at the wing root, transitioning to an NACA 64-616 section at the wingtip. The A-15 carries 50 kg (110 lb) of water ballast. The landing gear is a retractable monowheel. [1] [2]

A total of 350 A-15s were built. [1]

Operational history

The A-15 was used to set many world records, including a world goal distance record of 714.023 km (444 mi), flown in June 1960. [1]

In August 2011, there was one A-15 registered with the Federal Aviation Administration in the United States. [3]

Specifications (Antonov A-15)

Data from The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II [4] Sailplane Directory [1]

General characteristics

Performance

See also

Related development

Related lists

Notes

  1. 1 2 3 4 5 6 Activate Media (2006). "A-15 Antonov". Archived from the original on 29 August 2012. Retrieved 8 August 2011.
  2. Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on 19 July 2011. Retrieved 8 August 2011.
  3. Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Archived from the original on 17 September 2012. Retrieved 15 August 2011.
  4. Shenstone, B.S.; K.G. Wilkinson (1963). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 245–246.

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References