| Technical data | |
|---|---|
| Type | I-17 TsKB-19 |
| Function | fighter |
| Year | 1935 |
| Crew | 1 |
| Engines | 1*750hp M-100 |
| Speed | 500km/h |
| Ceiling | 11000m |
| Range | 800km |
| Armament | 4*mg7.62mm |
The I-17 was a sleek fighter with a water-cooled engine, built for comparison with the stubby radial-engined I-16.
Few built, some used in combat in 1941.
There was a widely used argument against evaporative cooling systems - vulnerability. But... this is a common feature of water-cooled engines (except special cases with armor-shielded cooler like Il-2). Large area of cooling surface is not a weakness - higher probability of combat damage is compensated by relatively lower impact of a hole on the system.
During trials of Stal-6 A.B.Yumashev performed few flights with imitation of a cooler combat damage. Each flight lasted more than 30min! Taking into account that flight endurance of (most) Soviet WW-II single-engine fighters was close to 1hour, damaged fighter could not only return home safely, but do it after the fight is over.
There also was a room for improvement - Stal-6 had single-unit cooler, while segmented system could be even less sensitive to damage.
TsKB-15 - the first prototype;
TsKB-33 used evaporative cooling. Cancelled;
| Modified January 25, 1996 |
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