Nieuport 23 C1
| GENERAL DATA | |||
| Type |
Fighter, Trainer
|
||
| Manufacturer(s) | Nieuport |
||
| Prototype first flight | 1916 |
Introduction | Early 1917 |
| Production | ? |
Crew | 1 |
| DIMENSIONS | |||
| Length | 6.40 m |
Empty Weight | 355 kg |
| Wingspan | 8.20 m (upper) |
Loaded Weight | 574 kg |
| Height | 2.40 m |
Max takeoff weight | ? kg |
| Wing area | 14.75 m² |
Wing loading | 38.915 kg/m² |
| ARMAMENT | ||||
| Guns | 1× 0.303 in (7.7 mm) Vickers |
Ammunition Carried |
? |
|
- |
- |
|||
| Other Armament | 8 x Le Prieur rockets intended
for the destruction of Drachens |
|||
(*) forward firing, synchronized
| POWERPLANT | |||
| Engine | 1 ×
Le Rhône 9Jb |
Type & Displacement | 9 cylinder rotary engine, 15 L
|
| Horsepower | 120 hp |
Power/Weight Ratio | 209.06 hp / ton * |
| Fuel Capacity | 53 L
|
||
(*) with the loaded weight
| PERFORMANCES | |||
| Maximum Speed | 168 km/h |
Rate of Climb | 5.8 m/s |
| Range | 250 km |
Service Ceiling | 6500 m |
| Sources | |||
| Wikipédia | - |
- | |
Drawings |
