Caudron-Renault CR.714.C1 Cyclone
| GENERAL DATA | |||
| Other Designation(s) | Caudron
C.714.C1 Cyclone |
||
| Type | Light Fighter |
Crew | 1 |
| Manufacturer(s) | Caudron-Renault |
||
| Production | 90 (1939-1940
) |
||
| First Flight | 18 July 1936 (C.710) 6 July 1938 |
Introduction | 1940 |
| DIMENSIONS | |||
| Length | 8.63 m |
Empty Weight | 1395 kg |
| Wingspan | 8.97 m |
Loaded Weight | 1880 kg |
| Height | 2.87 m |
Max takeoff weight | ? kg |
| Wing area | 12.5 m² |
Wing Loading | 140 kg/m² |
| ARMAMENT | |||
| Main Guns | 4× 7.5 mm (0.295 in) M39 MAC
1934* |
Ammunition Carried | 4 x 300 |
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | - |
||
(*) mounted in wings
| POWERPLANT | |||
| Engine | 1 × Renault 12R-03 |
Type & Displacement | V-12 air-cooled inverted , 19 L
|
| Horsepower (maximum) | 500
hp |
Power/Weight Ratio | 265.96 hp / ton * |
| Fuel Capacity | 205 L
|
||
(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 488 km/h at 5000 m |
Cruising Speed | 320 km/h |
| Stall Speed * | 117 km/h |
Service Ceiling | 9400 m |
| Rate of Climb | 10 m/s |
Range | 900 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
