Nieuport 21
| GENERAL DATA | |||
| Type |
Fighter-Trainer, Fighter
|
||
| Manufacturer(s) | Nieuport |
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| Prototype first flight | 1916 |
Introduction | 1916 |
| Production | ? |
Crew | 1 |
| DIMENSIONS | |||
| Length | 5.80 m |
Empty Weight | 350 kg |
| Wingspan | 7.80 m (lower), 8.16 m (upper) |
Loaded Weight | 530 kg |
| Height | 2.40 m |
Max takeoff weight | ? kg |
| Wing area | 14.75 m² |
Wing loading | 367.271 kg/m² |
| ARMAMENT | ||||
| Guns | 1× 0.303 in (7.7 mm) Lewis
MG * |
Ammunition Carried |
? |
|
- |
- |
|||
| Other Armament | ? |
|||
(*) forward firing
| POWERPLANT | |||
| Engine | 1 ×
Le Rhône 9C |
Type & Displacement | air-cooled rotary engine, 10.89
L |
| Horsepower | 80 hp |
Power/Weight Ratio | 150.94 hp / ton * |
| Fuel Capacity | 53 L
|
||
(*) with the loaded weight
| PERFORMANCES | |||
| Maximum Speed | 152 km/h |
Rate of Climb | 4.16 m/s |
| Range | 250 km |
Service Ceiling | 5200 m |
| Sources | |||
| Wikipédia | - |
- | |
Drawings |
