| Technical data | ||
|---|---|---|
| Type | S-10 Gnome | S-10 Argus |
| Function | Reconnaissance | |
| Year | 1913 | |
| Crew | 3 | ? |
| Engines | 1*80hp Gnome | 1*100hp Argus |
| Length | 8.0m | - |
| Wing Span | 16.9m/12.0m | 13.7m/8.8m |
| Wing Area | 46.0m2 | 35.5m2 |
| Empty weight | 567kg | 550kg |
| Loaded weight | 1011kg | 850kg |
| Wing Load (kg/m2) | 22 | 24.3 |
| Power load (kg/hp) | 12.7 | 8.5 |
| Maximum Speed at 0m | 99km/h | - |
| Climb to 500m | 5min 20s | - |
| Range | 500km | - |
|
Designation S-10 was used for 16 similar airplanes, closely resembling the S-6. S-10 had less powerful engine and generally weaker structure. Two seats were placed side-by-side, and controls could be moved between crew members.
|
On airplane contest in 1913 this aircraft piloted by G.V.Alekhnovich set Russian record : 500km non-stop flight, staying airborne for 4h56min and 12 seconds. S-10 won the contest, despite as military aircraft it was weaker than S-6A and S-6B, slower and less maneuverable. Its payload 45-48% of aircraft weight was exceptional.
Following year this aircraft was rebuilt for 100hp Gnome Monosaupape engine, and smaller wing. Two S-10 were powered by 100hp Argus engine.
| Modified September 4, 1997 |
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