Polikarpov I-17 (TsKB-19bis)
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type | Fighter |
Crew | 1 |
| Manufacturer(s) | Polikarpov |
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| Production | 3 (TsKB-19bis) |
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| First Flight | 1 September 1934 |
Introduction | - |
| Variants | |||
| 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. | ||
| DIMENSIONS | |||
| Length | 7.30 m | Empty Weight | 1533 kg |
| Wingspan | 10.19 m |
Loaded Weight | ? kg |
| Height | 2.56 m |
Max takeoff weight | 1930 kg |
| Wing area | 17,70 m² |
Wing Loading | 176,50 kg/m² |
| ARMAMENT | |||
| Main Guns | 1 x 20mm ShVAK cannon * |
Ammunition Carried | 1 x ? |
| Secondary Guns | 4 x 7.62 mm (0.300 in) ShKAS MG ** |
Ammunition Carried | 4 x ? |
| Other Armament | 2 x 100 kg bombs under the wings |
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(*) noose, (**) wings
| POWERPLANT | |||
| Engine | 1 × Klimov M-100 |
Type & Displacement | supercharged liquid-cooled 60° V12 , 36 L |
| Horsepower (maximum) | 860
hp |
Power/Weight Ratio | 445,59 hp / ton * |
| Fuel Capacity | ?
|
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(*) with takeoff weight
| PERFORMANCES | |||
| Maximum Speed | 490 km/h |
Cruise Speed | 440 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 11000 m |
| Rate of Climb | ? m/s |
Range | 800 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | Aviastar | - |
|
Drawings |
