Jump to content

Polikarpov I-17

From Wikipedia, the free encyclopedia
(Redirected from TsKB-33)
Polikarpov I-17
Role Single-seat fighter
National origin Soviet Union
Manufacturer Polikarpov
First flight 1 September 1934
Number built 3

The Polikarpov I-17 was a Soviet single-seat fighter prototype designed and built by a team headed by Nikolai Polikarpov at the Central Design Bureau (TsKB) in 1934.

Development

[edit]

The I-17 was a lightweight single-seat low-wing cantilever monoplane. Developed under the design bureau designation TsKB-15 it first flew on 1 September 1934 powered by a 567 kW (760 hp) Hispano-Suiza 12 Ybrs engine. The second prototype designated the TsKB-19 had a revised inward retracting wide-track main landing gear and a Soviet M-100 engine. This second prototype was displayed at the 1936 Salon de l'Aeronautique in Paris. The third prototype designated the TsKB-33 had reduced armament to save weight and a revised engine cooling system, but the further development was abandoned in 1936.

A number of related unbuilt projects were also under development including the I-17Z parasite fighter under the designations TsKB-25 with a M-34RNF engine and the TsKB-43 with a Hispano-Suiza engine, none were built.

Variants

[edit]
TsKB-15
First prototype I-17 powered by a 567 kW (760 hp) Hispano-Suiza 12 Ybrs engine.
TsKB-19
Second revised I-17 prototype powered by a M-100 engine.
TsKB-25
Unbuilt I-17Z project for a Mikulin AM-34RNF powered parasite fighter.
TsKB-33
Third revised I-17 prototype with reduced armament.
TsKB-43
Unbuilt project with a Hispano-Suiza engine.

Surviving aircraft

[edit]

One I-17 prototype is on display at the V. P. Chkalov Memorial Museum in Chkalovsk, Russia. [1]

Specifications (TsKB-19)

[edit]

General characteristics

  • Crew: 1 (pilot)
  • Length: 7.30 m (23 ft 11 in)
  • Wingspan: 10.19 m (33 ft 5 in)
  • Height: 2.56 m (8 ft 5 in)
  • Gross weight: 1,930 kg (4,250 lb)
  • Powerplant: 1 × Klimov M-100 engine , 632 kW (860 hp)

Performance

  • Maximum speed: 490 km/h (305 mph, 265 kn)
  • Range: 800 km (497 mi, 432 nmi)
  • Service ceiling: 11,000 m (36,090 ft)

Armament

  • 1 x 20mm ShVAK cannon
  • 4 x 7.62mm ShKAS machine guns
  • 2 x 100kg bombs under the wings

Notes

[edit]
  1. ^ "Memorial Museum of V.P. Chkalova". Museum.ru. Retrieved 21 January 2023.

References

[edit]
  • Angelucci, Enzo (1980). The Rand McNally Encyclopedia of Military Aircraft. Rand McNally Publishing. p. 183.
  • Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft 1875-1995. London: Osprey. ISBN 1-85532-405-9.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
[edit]