| Type | Helicopter | |
| Company | Sikorsky Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
27.0
88.7
|
|
| Height (m) |
0.6
7.6
50.1
|
|
| Rotors | ||
| Main rotor diameter (m) |
1.2
22.0
62
|
|
| Tail rotor diameter (m) |
0.8
4.9
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
10,740
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
19,050.9
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
2 pilots, 1 or more crew chiefs |
| Speeds | ||
| Max. Speed (km/h) |
25
315
28,165
|
|
| Сruise Speed (km/h) |
52
1,000
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
2,385
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
7,850
60,000
|
2 powerplants 3925 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
3,565
161,544
|
|
| Static ceiling (m) |
3
3
5,485
|
2 pilots, 1 or more crew chiefs |
| Range (Ferry range) (km) |
4
1,000
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
5,105.4
36,000
|
|
| Stat | ||
| Introduction | 1964 | |
| First flight | 14.10.1964 | |
| Stop production | 2012 | |
