Nieuport 25
| GENERAL DATA | |||
| Type |
Fighter, Advanced Trainer
|
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| Manufacturer(s) | Nieuport |
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| Prototype first flight | 1917 |
Introduction | 1917 |
| Production | ? |
Crew | 1 |
| Variants | |||
| Nieuport 24 C.1 | single seat fighter | ||
| Nieuport 24 E.1 | unarmed single seat fighter-trainer, often fitted with an 80 hp Le Rhône 9C | ||
| Nieuport 24bis C.1 | similar to 24 but used earlier metal tail with a comma shaped rudder and an angular horizontal tail. | ||
| Nieuport 24bis E.1 | unarmed single seat fighter-trainer, often fitted with an 80 hp Le Rhône 9C | ||
| Nieuport 25 C.1 | Similar to 24 or 27, but with larger 200 hp Clerget rotary. Very few produced. | ||
| Nieuport 26 C.1 | Development of 24, powered by Hispano-Suiza V-8 engine. | ||
| Nakajima 3 (Ko 3) | Japanese designation for locally-built Nieuport 24/27. | ||
| Nieuport B.Kh2 | Siamese designation for Nieuport 24bis. | ||
| DIMENSIONS | |||
| Length | 5.88 m |
Empty Weight | 355 kg |
| Wingspan | 7.82 m (lower) / 8.21 m (upper) |
Loaded Weight | 547 kg |
| Height | 2.44 m |
Max takeoff weight | ? kg |
| Wing area | 14.75 m² |
Wing loading | 36.88 kg/m² |
| ARMAMENT | ||||
| Guns | 1× 0.303 in (7.7 mm) Vickers
MG * |
Ammunition Carried |
? |
|
1× 0.303 in (7.7 mm) Lewis MG ** |
? |
|||
| Other Armament | - |
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(*) forward firing, synchronized except on RFC examples, (**) optionally mounted above the top wing.
| POWERPLANT | |||
| Engine | 1 ×
Clerget 11E |
Type & Displacement | rotary |
| Horsepower | 200 hp |
Power/Weight Ratio | 367 hp / ton * |
| Fuel Capacity | 95 L
|
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(*) with the loaded weight
| PERFORMANCES | |||
| Maximum Speed | 187 km/h |
Rate of Climb | 5.8 m/s |
| Range | 250 km |
Service Ceiling | 5500 m |
| Sources | |||
| Wikipédia (fr) | - |
- | |
Drawings |
