Type | Aircraft | |
Company | Short Brothers | |
Scheme | High wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
41.6
88.7
|
|
Height (m) |
0.6
14.3
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
229.1
925
|
|
Wingspan (Beam) (m) |
0.1
48.4
95
|
|
Aspect ratio |
1.7
10.2
25.6
|
|
Weights | ||
Empty weight (kg) |
8
57,606.2
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
104,326.3
575,000
|
|
Capacity | ||
Crew (per.) |
1
5
112
|
two pilots, engineer, navigator and loadmaster |
Payload (kg) |
23
35,380.2
122,470
|
|
Capacity passengers (per.) |
1
150
400
|
|
Speeds | ||
Max. Speed (km/h) |
25
566
28,165
|
|
Сruise Speed (km/h) |
52
576
3,087
|
at 7315 m |
Stall Speed (km/h) |
40
180
257.7
|
|
Fuel | ||
Fuel Capacity (l) |
23
45,869
320,000
|
|
Power | ||
Total Power (hp) |
0.4
22,920
60,000
|
4 powerplants 5730 hp each |
Performance | ||
Service ceiling (m) |
0.6
9,144
161,544
|
|
Range (Ferry range) (km) |
4
8,528
40,700
|
with maximum fuel |
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
323.1
36,000
|
|
Stat | ||
Number built (qt) |
0
10
43,000
|
|
Introduction | 1964 | |
First flight | 05.01.1964 | |
Stop production | 1976 |