Westland Westminster
The Westland Westminster was a project by the British company Westland Aircraft for a transport helicopter . It was based on basic elements of the Sikorsky S-56 . Development was stopped in early 1960.
Technical specifications
Parameter | Data |
---|---|
Construction year | 1958 |
Manufacturer | Westland Aircraft |
Rotor diameter | 21.95 m |
length | 27.40 m |
height | 5.04 m |
Takeoff mass | 16345 kg |
crew | 3 |
Top speed | 185 km / h |
Range | 330 km |
Engine | 2 × Napier Eland 229A shaft drive , each 2059 kW (2800 PS) |
See also
literature
- Giorgio Apostolo: World Cyclopedia of Airplanes, Volume 3 , Südwest-Verlag, Munich 1984, ISBN 3-517-00851-6 .