Bristol Greek and Bulgarian Tourers Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
December 1923 |
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Greek Tourer: |
6 - The Bristol Aeroplane Co. Ltd |
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Bulgarian Tourer: |
5 - The Bristol Aeroplane Co. Ltd |
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Type Specification | |
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Applies to: |
Greek Tourer |
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Type: |
Two seat touring biplane |
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Wing: |
Two bay biplane. Wing has no sweep and dihedral on all planes. Ailerons on all planes |
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Fuselage: |
Fuselage mounted between the wings, rectangular section, tapering sharply to the rear. |
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Tail Unit: |
Tailplane and elevator mounted mid fuselage, fin and rudder below and above fuselage |
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Landing Gear: |
Crossaxle main gear supported on main legs with radius rod to rear. Tail skid |
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Power Plant: |
One 230 hp Siddeley Puma |
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Accommodation: |
Tandem cockpits for two crew |
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Dimensions | |
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Span: |
39 ft 5 in |
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Length: |
26 ft |
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Height: |
10 ft |
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Wing Area: |
407 sq ft |
Weights | |
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Empty: |
1,750 lb |
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All-up: |
2,800 lb |
Performance | |
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Max Speed: |
120 mph |
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Endurance: |
5 hours |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |