Westland Westminster

from Wikipedia, the free encyclopedia
Westland Westminster
Westland Westminster Westland Westminster
Type: medium-weight transport helicopter
Design country:

United KingdomUnited Kingdom United Kingdom

Manufacturer:

Westland Aircraft

First flight:

June 15, 1958

Commissioning:

-

Production time:

1958-1959

Number of pieces:

2

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 .