Miles Miles Kestrel Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
3 June 1937 |
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M.9 Kestrel: |
1 - Phillips & Powis, Woodley |
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Type Specification | |
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Applies to: |
Miles M.9 Kestrel |
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Type: |
Private venture advanced trainer, later developed into Master |
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Wing: |
Low wing cantilever monoplane of spruce structure covered in plywood. Split flaps fitted as standard |
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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: |
Single wheel on each main leg, which retract into wing. Tailwheel |
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Power Plant: |
One 745 hp Rolls-Royce Kestrel XVI engine in nose |
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Accommodation: |
Tandem seats for crew in enclosed cockpit |
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Dimensions | |
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Span: |
39 ft |
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Length: |
30 ft 6 in |
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Height: |
9 ft 5 in |
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Wing Area: |
235 sq ft |
Weights | |
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Empty: |
4,160 lb |
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All-up: |
5,340 lb |
Performance | |
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Max Speed: |
296 mph at 14,500 ft |
Preserved in British Museums | |
None known | |
Web Sites | |
http://www.jaapteeuwen.com/ww2aircraft/html%20pages/MILES%20M9%20KESTREL.htm | |