![]() |
|
Role | Single-seat fighter |
---|---|
National origin | Soviet Union |
Manufacturer | Polikarpov |
First flight | 1 September 1934 |
Number built | 3 |
|
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.
Ceiling
Combat RANGE
Aircraft Speed
Max Crew
|
---|
The Polikarpov I-17 was a light weight fighter developed in the USSR during the 1930s. It’s performance was better then most contemporary fighters but authorities preferred the radial engined I-16 so the I-17 was not developed. The Polikarpov I-17 was designed in the early 1930s to be powered by the Hispano-Suiza 12 Yhrs in-line engine.
The first prototype made its maiden flight on 1 September 1934 and reached a speed of 455 km/h, climbed rapidly and was judged superior to the contemporary I-16
The second prototype, with several improvements, first flew in early 1935 and the third prototype began flying in 1936.