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Sikorsky S-17
Type of aircraft From Wikipedia, the free encyclopedia
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The Sikorsky S-17 was a Russian single engine aircraft built at the Russian Baltic Railroad Car Works in Petrograd while Igor Sikorsky was the chief engineer of the aircraft manufacturing division.
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Design and development
The S-17 was a two seat reconnaissance biplane based on the S-10 and powered by a Sunbeam Crusader V-8 water-cooled engine rated at 150 hp (112 kW).[1][2]
Specifications

Data from Russian Aviation Museum[1]
General characteristics
- Crew: Two
- Length: 24 ft 7 in (7.5 m)
- Upper wingspan: 45 ft 3 in (13.8 m)
- Lower wingspan: 41 ft 0 in (12.5 m)
- Wing area: 468 sq ft (43.5 m2)
- Empty weight: 1,863 lb (845 kg)
- Gross weight: 2,624 lb (1,190 kg)
- Powerplant: 1 × Sunbeam Crusader V-8, side-valve, water-cooled, piston engine, 150 hp (110 kW)
- Propellers: 2-bladed
Performance
- Wing loading: 5.6 lb/sq ft (27.4 kg/m2) max load
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References
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