| Type | Helicopter | |
| Company | Sikorsky Aircraft Corporation | |
| Operation | Passenger Cargo | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
18.0
88.7
|
|
| Height (m) |
0.6
5.3
50.1
|
|
| Rotors | ||
| Disc area (m2) |
1.4
280.6
460
|
|
| Main rotor diameter (m) |
1.2
18.9
62
|
|
| Tail rotor diameter (m) |
0.8
3.2
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
5,595
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
8,618.3
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
pilots |
| Capacity passengers (per.) |
1
30
400
|
up to 30 passengers |
| Speeds | ||
| Max. Speed (km/h) |
25
267
28,165
|
|
| Сruise Speed (km/h) |
52
222
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
3,180
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
3,000
60,000
|
2 powerplants 1500 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
3,810
161,544
|
|
| Static ceiling (m) |
3
2,150
5,485
|
|
| Range (Ferry range) (km) |
4
833
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
676.7
36,000
|
400–670 m/min |
| Stat | ||
| Number built (qt) |
0
119
43,000
|
|
| Introduction | 01.09.1961 | |
| First flight | 11.03.1959 | |
