Westland Westminster Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
15 June 1958 |
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Westminster: |
2 - Westland Aircraft Ltd, Yeovil |
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Type Specification | |
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Applies to: |
Westland Westminster |
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Type: |
Transport or heavy lift helicopter |
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Rotor System: |
Five bladed main rotor. One four blade anti torque and steering rotor |
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Fuselage: |
Tapering rectangular section fuselage of four longerons and twelve rectangular frames built of metal covered in plastic |
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Landing Gear: |
Fixed tricycle type |
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Power Plant: |
Two 2,920 shp Napier Eland E220 turboshafts mounted above cabin |
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Accommodation: |
Two crew on enclosed flight deck plus two observers. Planned cabin for 40 passengers |
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Dimensions | |
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Rotor Diameter: |
72 ft 0 in |
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Length: |
86 ft 9 in |
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Height: |
21 ft 1 in |
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Wing Area: |
4,069 sq ft |
Weights | |
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Empty: |
21,245 lb |
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Loaded: |
33,000 lb |
Performance | |
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Max Speed: |
155 mph |
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Rate of Climb: |
1,750 ft/min at sea level |
Preserved in British Museums | |
None known | |
Web Sites | |