Manufacturer | Caudron |
Model | C.81 |
Modification | C.81 |
Country | France |
Years | 1923 |
Type | Transport aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 26.30 m |
Length | 16.00 m |
Height | 4.85 m |
Wing area | 145.00 m2 |
Zero fuel weight | - |
Empty weight | 4271 kg |
Maximum takeoff weight | 6360 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Lorraine-Dietrich +2 Salmson CM.9 |
Power | 1 x 400 + 2 x260 HP |
Thrust | - |
Maximum speed | 145 km/h |
Cruising speed | 125 km/h |
Rate of climb | - |
Practical range | 450 km |
Service ceiling | 3700 m |
Hovering ceiling | - |
Crew | 2 |