Polikarpov P-2

The Polikarpov P-2 was a 1920s Soviet two-seat intermediate training biplane.[1] It was a single-bay biplane powered by a 300 hp (224 kW) M-6 water-cooled V-8 engine (Hispano-Suiza 8Fb) with a retractable radiator.[1] The prototype first flew in 1927 and entered production with an order for 55 for use as an intermediate trainer.[1] Problems with the original strut-based wing bracing resulted in many aircraft being modified to use bracing wires. It was one of the first aircraft types to be used to train navigators and machine gunners but the type was not very stable and had problems with flying qualities causing the type to be little used.[2]

Polikarpov P-2
Role Training biplane
National origin Soviet Union
Manufacturer Polikarpov
First flight 1927
Number built 55+

Specifications

Data from [1]The Illustrated Encyclopedia of Aircraft

General characteristics

  • Crew: 2
  • Wingspan: 10.40 m (34 ft 1.5 in)
  • Powerplant: 1 × M-6 water-cooled V-8 piston engine , 224 kW (300 hp)

Performance

  • Maximum speed: 206 km/h (128 mph, 111 kn)

Armament

  • ring-mounting on rear-cockpit for a DA machine-gun

Related lists

References

Notes
  1. Orbis 1985, p. 2756
  2. Vaclav 1986, pp. 226-227

Bibliography
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
  • Nemecek, Vaclav (1986). The History of Soviet Aircraft from 1918. London: Willow Books. ISBN 0-00-218033-2.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.