Gloster Gnatsnapper Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
February 1928 |
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Gnatsnapper I: |
2 - Gloster Aircraft |
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Gnatsnapper II: |
2 - Gloster Aircraft (converted from mark I) |
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Gnatsnapper III: |
1 - Gloster Aircraft (converted from mark II) |
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Type Specification | |
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Applies to: |
Gloster Gnatsnapper I |
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Type: |
Deck-landing fighter to specification N.21/26 |
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Wing: |
Single bay biplane with staggered, unswept, unequal span wings of metal structure with fabric covering. Ailerons on all four wings |
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Fuselage: |
Round fuselage mounted on lower wing of metal structure with fabric covering |
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Tail Unit: |
Wire braced tailplane at base of single fin with balanced rudder and elevators |
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Landing Gear: |
Crossaxle type main gear attached to fuselage by oleo legs and radius rods. Tail skid |
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Power Plant: |
One 450 hp Bristol Mercury IIA nine-cylinder air-cooled radial in the nose driving a two blade wooden propeller |
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Accommodation: |
Pilot in open cockpit aft of wing |
Armament: |
Two Vickers guns in troughs on the fuselage sides |
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Dimensions | |
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Span: |
33 ft 6 in |
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Length: |
24 ft 7 in |
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Height: |
10 ft 11 in |
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Wing Area: |
360 sq ft |
Weights | |
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Empty: |
2,970 lb |
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Loaded: |
3,625 lb |
Performance | |
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Max Speed: |
165 mph at 10,000 ft |
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Climb: |
12.2 min to 15,000 ft |
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Service Ceiling: |
20,500 ft |
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Duration: |
5 hr at 15,000 ft |
Preserved in British Museums | |
None known | |
Web Sites | |