| 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 | |
