Company | Boeing | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
46.6
88.7
|
41,25 m - 46,61 m depending on variant |
Height (m) |
0.6
12.9
50.1
|
or 12,65 depending on variant |
Wings | ||
Wingspan (Beam) (m) |
0.1
44.4
95
|
or 39,9 depending on variant |
Weights | ||
Empty weight (kg) |
8
66,406
276,800
|
46785 kg - 66406 kg depending on variant |
Max. takeoff weight (Gross weight) (kg) |
154
151,320
575,000
|
100800 kg - 151320 kg depending on variant |
Capacity | ||
Crew (per.) |
1
4
112
|
Pilot, Co-Pilot, Flight Engineer, Navigator |
Capacity passengers (per.) |
1
189
400
|
110-189 depending on variant |
Speeds | ||
Сruise Speed (km/h) |
52
972
3,087
|
or 1000 km/h depending on variant |
Fuel | ||
Fuel Capacity (l) |
23
90,160
320,000
|
60900 l - 90160 l depending on variant |
Power | ||
Thrust (kN) |
1.5
337.6
1,914
|
4 powerplants 84,4 kN each (or 53,3 kN, or 75,6 kN depending |
Performance | ||
Range (Ferry range) (km) |
4
6,920
40,700
|
or 6820 km depending on variant (max. payload) |
Landing roll (m) |
20
1,813
2,570
|
1740 m - 1813 m depending on variant |
Stat | ||
Number built (qt) |
0
154
43,000
|
|
First flight | 23.11.1959 | |
Stop production | 29.09.2010 |