Bristol Jupiter-Fighter and Advanced Trainers Aircraft
| |
Production Details | |
Design Company: |
|
First Flight: |
June 1923 |
Fighter: |
3 - The Bristol Aeroplane Co. Ltd |
Type 89 Trainer: |
9 - The Bristol Aeroplane Co. Ltd |
Type 89A Trainer: |
14 - The Bristol Aeroplane Co. Ltd |
Type Specification | |
Applies to: |
Bristol Type 89 Trainer |
Type: |
Two seat advanced training biplane |
Wing: |
Two bay staggered unswept biplane |
Fuselage: |
Box fuselage tapering to rear mounted mid gap to wings |
Tail Unit: |
Balanced rudder and elevators with wire braced fin above and below fuselage and tailplane |
Landing Gear: |
Crossaxle type carried on oleo legs with radius rods |
Power Plant: |
One 320 hp Bristol Jupiter IV |
Accommodation: |
Tandem cockpits for two crew |
Armament: |
None |
Dimensions | |
Span: |
39 ft 3 in |
Length: |
25 ft |
Height: |
9 ft 6 in |
Wing Area: |
405 sq ft |
Weights | |
Empty: |
2,326 lb |
All-up: |
3,250 lb |
Performance | |
Max Speed: |
110 mph |
Range: |
340 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known |