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 |