Boulton & Paul Bodmin Aircraft
| |
Production Details | |
|
Design Company: |
|
|
First Flight: |
Early 1924 |
|
P.12 Bodmin: |
2 - Boulton & Paul |
|
Type Specification | |
|
Applies to: |
Boulton & Paul P.12 Bodmin |
|
Type: |
Experimental aircraft to Air Ministry specification |
|
Wing: |
Three bay biplane with unstaggered, unswept, equal span wings. Metal structure with fabric covering. Ailerons on upper wing only |
|
Fuselage: |
Flat sided fuselage mounted on lower wing of all metal structure with fabric covering |
|
Tail Unit: |
Braced tailplane with single fin and rudder |
|
Landing Gear: |
Crossaxle type main gear mounted on oleo legs with smaller wheels forward to prevent nosing over. Tailskid |
|
Power Plant: |
Two 450 hp Napier Lions mounted in the fuselage driving two two bladed puller propellers and two four bladed pusher propellers mounted on the wing inboard struts |
|
Accommodation: |
Open cockpit forward of wongs for pilot with nose and dorsal gun positions |
Armament: |
Lewis gun at each gun position |
|
Dimensions | |
|
Span: |
70 ft |
|
Length: |
53 ft 4 in |
|
Height: |
Unknown |
|
Wing Area: |
1,204 sq ft |
Weights | |
|
Empty: |
7,920 lb |
|
Loaded: |
11,000 lb |
Performance | |
|
Max Speed: |
116 mph at sea level |
|
Climb: |
8 min 9 sec to 6,500 ft |
|
Service Ceiling: |
16,000 ft |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |