| Type | Aircraft | |
| Company | Bristol Aeroplane Company | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
54
88.7
|
|
| Height (m) |
0.6
15
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
494.0
925
|
|
| Wingspan (Beam) (m) |
0.1
70
95
|
|
| Wing loading (kg/m2) |
3.1
270
829
|
|
| Weights | ||
| Empty weight (kg) |
8
65,816.3
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
131,541.8
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
12
112
|
6-12 |
| Capacity passengers (per.) |
1
100
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
480
28,165
|
at 7 620 m |
| Сruise Speed (km/h) |
52
402
3,087
|
at 7 620 m |
| Fuel | ||
| Fuel Capacity (l) |
23
61,971
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
21,200
60,000
|
8 powerplants 2650 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
7,620
161,544
|
at full weight |
| Range (Ferry range) (km) |
4
8,900
40,700
|
at 7 620 m |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
228.6
36,000
|
at sea level |
| Propellers | ||
| Propellers (qt) |
1
8
8
|
paired contra-rotating Rotol |
| Prop diameter (m) |
1.8
4.9
5.8
|
|
| Prop blade number (qt) |
1
3
8
|
per propeller (6 per pair) |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1949 | |
| First flight | 04.09.1949 | |
| Stop production | 1953 | |
