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