Fairey Gyrodyne Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
7 December 1947 |
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Gyrodyne: |
2 - Fairey |
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Jet Gyrodyne: |
1 - Fairey (converted from Gyrodyne) |
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Type Specification | |
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Applies to: |
Fairey Gyrodyne |
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Type: |
Light compound helicopter |
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Rotor System: |
Three blade main rotor driven. No tail rotor |
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Fuselage: |
All metal fuselage with short wings mounted on side to relieve load on rotor during forward flight |
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Tail Unit: |
Tailplane mounted at rear of fuselage with twin fins at tip |
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Landing Gear: |
Fixed tricycle undercarriage. Nose wheel under fuselage. Main wheels under wing |
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Power Plant: |
One Alvis Leonides nine cylinder radial in fuselage driving main rotor and propeller on starboard wing tip |
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Accommodation: |
Enclosed cabin |
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Dimensions | |
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Rotor Diameter: |
51 ft 9 in |
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Length: |
25 ft |
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Height: |
10 ft 2 in |
Weights | |
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Empty: |
3,600 lb |
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Loaded: |
4,800 lb |
Performance | |
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Max Speed: |
140 mph |
Preserved in British Museums | |
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Jet Gyrodyne: |
XJ389 - Museum of Berkshire Aviation, Woodley - Display |
Web Sites | |
http://avia.russian.ee/helicopters_eng/fairey_gyrodyne-r.html | |