Miles Peregrine Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
12 September 1936 |
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M.8 Peregrine: |
2 - Phillips & Powis, Woodley |
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Type Specification | |
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Applies to: |
Miles M.8 Peregrine |
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Type: |
Twin engined cabin monoplane built as private venture |
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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: |
Retractable main gear, single main wheels retract rearwards into engine nacelles. Tail wheel |
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Power Plant: |
Two 205 hp de Havilland Gipsy Six II engines mounted on wing |
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Accommodation: |
Crew of two with seats for 6 passengers in enclosed cabin |
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Dimensions | |
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Span: |
46 ft |
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Length: |
32 ft |
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Height: |
9 ft 6 in |
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Wing Area: |
300 sq ft |
Weights | |
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Empty: |
3,350 lb |
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All-up: |
5,500 lb |
Performance | |
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Max Speed: |
180 mph |
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Rate of Climb: |
966 ft/min |
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Ceiling: |
23,000 ft |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |