Manufacturer | Gloster |
Model | Grebe |
Modification | Grebe Mk.II |
Country | United Kingdom |
Years | 1923 |
Type | Fighter |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 8.94 m |
Length | 6.17 m |
Height | 2.82 m |
Wing area | 23.60 m2 |
Zero fuel weight | - |
Empty weight | 769 kg |
Maximum takeoff weight | - |
Normal takeoff weight | 1151 kg |
Flight duration | 2.45 h |
Engine | 1 Armstrong Siddeley Jaguar IV |
Power | 1 x 400 HP |
Thrust | - |
Maximum speed | 243 km/h |
Cruising speed | 221 km/h |
Rate of climb | - |
Practical range | 610 km |
Service ceiling | 7010 m |
Hovering ceiling | - |
Crew | 1 |