| Type | Helicopter | |
| Company | Sikorsky Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
22.3
88.7
|
|
| Height (m) |
0.6
5.5
50.1
|
|
| Rotors | ||
| Main rotor diameter (m) |
1.2
18.9
62
|
|
| Blades per rotor (qt) |
4
5
5
|
|
| Tail rotor diameter (m) |
0.8
3.2
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
6,051
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
10,001.7
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Capacity passengers (per.) |
1
5
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
265
28,165
|
|
| Сruise Speed (km/h) |
52
248
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
2,585
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
3,000
60,000
|
2 powerplants 1500 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
5,334
161,544
|
|
| Static ceiling (m) |
3
3,700
5,485
|
|
| Range (Ferry range) (km) |
4
1,254
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
400
36,000
|
400-670 m/min |
| Stat | ||
| Introduction | 1961 | |
| First flight | 1959 | |
