Bristol Brabazon
Technical Specifications
| First Flight: |
September 4, 1949 |
| Number Built: |
2 were built for commercial use |
| Length: |
177 feet |
| Wing Span: |
230 feet |
| Height: |
50 feet |
| Max Take-Off Wt.: |
290,000 lbs. |
| Max Landing Wt.: |
N/A |
| Empty Wt.: |
N/A |
| Max Cruising Speed: |
N/A |
| Normal Cruising Speed: |
250 mph 217 kts |
| Stall Speed: |
N/A |
| Service Ceiling: |
34,500 feet |
| Fuel Capacity: |
N/A |
| Range: |
5500 miles |
| Fuel Type: |
115/145 octane |
| Fuel Consumption: |
N/A |
| Engines: |
8 Bristol Centaurus 20 rated @ 2500 HP each |
| Seating: |
100 passengers |
| Crew: |
12 Total |
Engine Specifications
Bristol Centaurus 20
|
| Type: |
18 cylinder radial air cooled radial |
| Diameter: |
N/A |
| Length: |
N/A |
| Bore: |
N/A |
| Stroke: |
N/A |
| Displacement: |
N/A |
| Compression Ratio: |
N/A |
| Dry Weight: |
N/A |
| Ignition: |
N/A |
| Fuel Grade: |
115/145 octane |
| Carburation: |
N/A |
| Performance: |
Take-Off Power 2500 HP |
|