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.
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
References
Fixed-wing aircraft (company designations) Fixed-wing aircraft (military designations) Helicopters (company designations) Helicopters (military designations) Experimental aircraft