Short S.31 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
19 September 1938 |
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S.31: |
1 - Short, Rochester |
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Type Specification | |
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Applies to: |
Short S.31 |
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Type: |
Experimental half scale Stirling |
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Wing: |
Plywood covered, two spar design mid wing cantilever monoplane |
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Fuselage: |
Plywood covered semi monocoque |
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Tail Unit: |
Cantilever monoplane type, all wooden with single fin and rudder |
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Landing Gear: |
Main wheels retract rearwards into inboard engine nacelles, tailwheel |
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Power Plant: |
Four 90 hp Pobjoy Niagara III engine on wingleading egde |
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Accommodation: |
Crew of two in tandem in enclosed cockpit |
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Dimensions | |
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Span: |
49 ft 7 in |
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Length: |
43 ft 7 in |
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Height: |
Unknown |
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Wing Area: |
325 sq ft |
Weights | |
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All-up: |
5,700 lb |
Performance | |
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Max Speed: |
184 mph |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |