The Polikarpov I-17 was a Soviet single-seat fighter prototype designed and built by a team headed by Polikarpov at the Central Design Bureau (TsKB)
| Polikarpov I-17 | |
|---|---|
| Role | Single-seat fighter Type of aircraft |
| 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.
General characteristics
Performance
Armament
Polikarpov aircraft | |
|---|---|
| Bombers | |
| Fighters/Interceptors | |
| Reconnaissance/Attack | |
| Airliners/Transports | |
| Trainers |
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Aircraft designed by TsKB | |
|---|---|
Soviet fighter designations, 1923–1940 | |
|---|---|
| Fighters (I) | |
| Two-seat fighter (DI) | |
| Multi-seat fighter (MI) |
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| Cannon fighter (IP) | |
| Descriptors | |
1 Not assigned | |