Miles Hawcon Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
29 November 1935 |
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M.6 Hawcon: |
1 - Phillips & Powis, Woodley |
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Type Specification | |
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Applies to: |
Miles M.6 Hawcon |
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Type: |
Experimental aircraft to research affect of wing thickness |
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Wing: |
Low wing cantilever monoplane of spruce structure covered in plywood. Split flaps fitted as standard. Four different sets of wings built to various thicknesses |
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Fuselage: |
Fuselage of spruce structure with plywood covering |
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Tail Unit: |
Cantilever tailplane with elevator at top of fuselage with single fin and rudder |
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Landing Gear: |
Two main wheels, each in aerodynamic fairing beneath wing. Tail skid |
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Power Plant: |
One 200 hp de Havilland Gipsy Six engine in the nose |
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Accommodation: |
Enclosed cabin above wing |
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Dimensions | |
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Span: |
33 ft |
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Length: |
25 ft |
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Height: |
6 ft 6 in |
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Wing Area: |
161 sq ft |
Weights | |
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Empty: |
1,550 lb |
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All-up: |
2,400 lb |
Performance | |
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Max Speed: |
181 mph |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |