Manufacturer | Leduc |
Model | Leduc 0.10 |
Modification | Leduc 0.10 |
Country | France |
Years | 1949 |
Type | Experimental aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 10.25 m |
Length | 10.52 m |
Height | 3.40 m |
Wing area | 16.00 m2 |
Zero fuel weight | - |
Empty weight | 1800 kg |
Maximum takeoff weight | - |
Normal takeoff weight | 3000 kg |
Flight duration | - |
Engine | 1 ПВРД Leduc |
Power | - |
Thrust | 1 x 2000 kN |
Maximum speed | 902 km/h |
Cruising speed | - |
Rate of climb | - |
Practical range | - |
Service ceiling | - |
Hovering ceiling | - |
Crew | 1 |