Gloster F.9/37 Aircraft
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Production Details | |
Design Company: |
|
First Flight: |
3 April 1939 |
F.9/37: |
2 - Gloster Aircraft Company |
Type Specification | |
Applies to: |
Gloster F.9/37 |
Type: |
Single-seat day and night fighter |
Wing: |
Low wing cantilever monoplane with unswept, tapered wings of all metal structure |
Fuselage: |
All metal fuselage |
Tail Unit: |
Tailplane mounted on top of fuselage with fins and rudders at each tip |
Landing Gear: |
Retractable main gear retract rearwards into engine nacelles. Tail wheel retracts into fuselage |
Power Plant: |
Two 1,050 hp Bristol Taurus T-S(a) fourteen-cylinder twin-row air-cooled radials driving three-blade propellers mounted on the wing |
Accommodation: |
Single seat for pilot in enclosed cockpit in the nose |
Armament: |
Two 20 mm Hispano cannon mounted in the nose |
Dimensions | |
Span: |
50 ft |
Length: |
37 ft |
Height: |
11 ft 7 in |
Wing Area: |
386 sq ft |
Weights | |
Empty: |
8,828 lb |
Loaded: |
11,615 lb |
Performance | |
Max Speed: |
360 mph at 15,000 ft |
Climb: |
19.6 min to 28,000 ft |
Service Ceiling: |
30,000 ft |
Preserved in British Museums | |
None known | |
Web Sites | |
http://www.jaapteeuwen.com/ww2aircraft/html%20pages/GLOSTER%20F9%2037.htm |