Vickers Vellore Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
17 May 1928 |
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Vellore I: |
1 - Vickers Ltd |
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Vellore III: |
1 - Vickers-Armstrongs Ltd |
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Vellore IV: |
1 - Vickers-Armstrongs Ltd |
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Type Specification | |
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Applies to: |
Vickers Type 134 Vellore I |
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Type: |
Civil freight and mail carrier to specification 34/24 |
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Wing: |
Two bay biplane. Wings are staggered and swept. Ailerons on all four wings |
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Fuselage: |
Fuselage mounted between wings of oval cross-section |
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Tail Unit: |
Biplane tailplane with four rudders |
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Landing Gear: |
Divided type gear. Main wheels carried on axle, shock absorber and radius rod attached to wing. Tailskid |
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Power Plant: |
One 525 hp Bristol Jupiter IX air-cooled radial engine in the nose |
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Accommodation: |
Crew of two in open cockpit ahead of the wing |
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Dimensions | |
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Span: |
76 ft |
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Length: |
51 ft 6 in |
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Height: |
16 ft 3 in |
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Wing Area: |
1,416 sq ft |
Weights | |
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Empty: |
4,796 lb |
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Gross: |
9,500 lb |
Performance | |
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Max Speed: |
114 mph at sea level |
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Initial Climb: |
515 ft/min |
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Range: |
350 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |