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 |