Folland Folland 43/37 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
1940 |
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43/37: |
12 - Folland |
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Type Specification | |
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Applies to: |
Folland 43/37 |
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Type: |
Flying engine test bed to Air Ministry Specification 43/37 |
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Wing: |
Low wing cantilever monoplane. Wing is of wooden structure with plywood covering |
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Fuselage: |
Semi-monocoque light alloy fuselage |
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Tail Unit: |
Tailplane and elevator at top of fuselage with single fin and rudder |
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Landing Gear: |
Fixed main gear with tail wheel |
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Power Plant: |
Various engines fitted including Sabre, Centaurus, Hercules and Griffon |
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Accommodation: |
Single seat for pilot in enclosed cockpit with cabin behind for two observers |
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Dimensions | |
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Span: |
58 ft |
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Length: |
43 ft 4 in |
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Height: |
16 ft 3 in |
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Wing Area: |
588 sq ft |
Weights | |
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Loaded: |
16,000 lb |
Performance | |
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Max Speed: |
Unknown |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |