Type | Helicopter | |
Company | Sikorsky Aircraft Corporation | |
Geometry | ||
---|---|---|
Length (m) |
1.9
21.5
88.7
|
|
Height (m) |
0.6
4.4
50.1
|
|
Rotors | ||
Main rotor diameter (m) |
1.2
62
62
|
|
Weights | ||
Empty weight (kg) |
8
9,840.0
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
11,814.7
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
2-3 |
Speeds | ||
Max. Speed (km/h) |
25
370
28,165
|
|
25
296
28,165
|
Max speed without auxiliary jets | |
Сruise Speed (km/h) |
52
258
3,087
|
|
Power | ||
Total Power (hp) |
0.4
2,800
60,000
|
2 powerplants 1400 hp each |
Thrust (kN) |
1.5
83.6
1,914
|
2 powerplants 41,8 kN each |
Performance | ||
Service ceiling (m) |
0.6
3,050
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
120.1
36,000
|
|
Stat | ||
Number built (qt) |
0
2
43,000
|
|
Introduction | 1976 | |
First flight | 12.10.1976 |