Polikarpov I-17

Moscow Aviation Plant No. 39 · Soviet Union · first flew 1934 · fighter

The Polikarpov I-17 was a Soviet single-seat fighter prototype of the mid-1930s, designed to explore the use of a liquid-cooled inline engine (Hispano-Suiza 12Y) in a clean low-wing monoplane airframe concurrent with the development of the radial-engined I-16. It demonstrated excellent performance but was not selected for production.

Recognition (WEFT)

W — WingsLow-mounted, tapered
E — Engines1 × piston, nose-mounted
F — Fuselage7.3 m fuselage
T — TailConventional

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Spot it by:

A slim low-wing monoplane with a long-nosed liquid-cooled engine, retractable undercarriage, and enclosed cockpit; the inline engine distinguishes it from the stubby radial-engined I-16 developed in parallel.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Designed by Nikolai Polikarpov's team and first flown in 1934, the I-17 achieved a high maximum speed for its era and impressed Soviet evaluators. However, logistical concerns about the imported Hispano-Suiza engine and the simultaneous success of the I-16 led to the cancellation of further development. Lessons from the I-17 influenced Soviet fighter design philosophy into the late 1930s.

Variants

Two prototype variants were built (TsKB-15 and TsKB-19), differing in engine fit and canopy arrangement.

Where you'll see it

Never entered operational service; used for state evaluation trials in 1934–1935.

Related aircraft

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