Westland Welkin Aircraft
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Production Details | |
Design Company: |
|
First Flight: |
1 November 1942 |
Welkin Prototype: |
2 - Westland Aircraft |
Welkin F.I: |
75 - Westland Aircraft |
Welkin NF.II: |
1 - Westland Aircraft (converted from F.I) |
Type Specification | |
Applies to: |
Westland Welkin F.I |
Type: |
High-altitude day fighter to specification F.4/40 |
Wing: |
Mid-wing cantilever monoplane of all metal construction and high aspect ratio. Unswept and tapers |
Fuselage: |
All metal oval fuselage |
Tail Unit: |
Single fin and rudder with tailplane and elevator mounted at base of fin |
Landing Gear: |
Main wheels retract rearwards into engine nacelles, tail wheel retracts forwards into fuselage |
Power Plant: |
Two 1,560 hp Rolls-Royce Merlin 61 twelve-cylinder V inline engines mounted in nacelles on the wing driving four bladed propellers |
Accommodation: |
Pilot in enclosed cockpit in nose |
Armament: |
Four Hispano 20 mm cannon under the fuselage nose |
Dimensions | |
Span: |
70 ft |
Length: |
41 ft 6 in |
Height: |
15 ft 3 in |
Wing Area: |
460 sq ft |
Weights | |
Empty: |
11,974 lb |
Max Take-off: |
19,775 lb |
Performance | |
Max Speed: |
387 mph at 26,000 ft |
Climb: |
20 min to 40,000 ft |
Service Ceiling: |
44,000 ft |
Range: |
1,480 miles |
Preserved in British Museums | |
None known | |
Web Sites | |