Miles Marathon Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
19 May 1946 |
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M.60 Marathon 1: |
2 - Miles Aircraft Ltd |
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M.69 Marathon 2: |
1 - Miles Aircraft Ltd |
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H.P.R.1 Marathon 1: |
40 - Handley Page |
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Type Specification | |
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Applies to: |
Handley Page (Reading) H.P.R.1 Marathon 1 |
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Type: |
Short range civil transport |
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Wing: |
High wing cantilever monoplane of all metal construction. Wing is unswept |
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Fuselage: |
All metal semi-monocoque unpressurised fuselage |
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Tail Unit: |
Cantilever tailplane with three fins and rudders constructed of metal |
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Landing Gear: |
Retractable tricycle design.Main gear retract into inner engine nacelles with nose gear retracting forward into fuselage |
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Power Plant: |
Four 340 hp de Havilland Gipsy Queen 70-3 engines in nacelles on wing |
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Accommodation: |
Crew of two with 18 passengers |
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Dimensions | |
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Span: |
65 ft |
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Length: |
52 ft 1.5 in |
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Height: |
14 ft 1 in |
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Wing Area: |
498 sq ft |
Weights | |
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Empty: |
11,688 lb |
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Maximum: |
18,250 lb |
Performance | |
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Speed: |
232 mph |
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Ceiling: |
18,000 ft |
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Range: |
935 miles |
Preserved in British Museums | |
None known | |
Web Sites | |