SPAD S.XIII C1
| GENERAL DATA | |||
| Type |
Fighter
|
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| Manufacturer(s) | SPAD |
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| Prototype first flight | 4 April 1917 |
Introduction | Late May 1917 |
| Production | 8472 |
Crew | 1 |
| DIMENSIONS | |||
| Length | 6.25 m |
Empty Weight | 601.5 kg |
| Wingspan | 8.25 m * |
Loaded Weight | 856.5 kg |
| Height | 2.60 m |
Max takeoff weight | ? kg |
| Wing area | 21.11 m² ** |
Wing loading | 27.97 to 40.594 kg/m² |
(*) late examples had a span of 8.08 m, (**) late examples had a wing area of 20.2 m2
| ARMAMENT | ||||
| Guns | 2× 0.303 in (7.7 mm) Vickers
MG * |
Ammunition Carried |
2 x 400,
500 |
|
| Other Armament | 4 x 11 kg bombs |
|||
(*) forward firing, synchronized, for USAS Examples, 2 x Marlin M1917 or M1918 machine guns
| POWERPLANT | |||
| Engine | 1 ×
Hispano-Suiza 8Ba, Bb or Bd |
Type & Displacement | Water cooled 8-cylinder vee-type,
11.76L |
| Horsepower | 200-220 hp |
Power/Weight Ratio | 233.51-256.86 hp / ton * |
| Fuel Capacity | 113 L
|
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(*) with the loaded weight
| PERFORMANCES | |||
| Maximum Speed | 211 km/h
at 1000 m 201 km/h at 4000 m |
Rate of Climb | 6.25 m/s |
| Range | 350 km |
Service Ceiling | 6800 m |
| Sources | |||
| Wikipédia | militaryfactory.com | ||
Drawings |
