| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
15.4
88.7
|
|
| Height (m) |
0.6
3.7
50.1
|
3,56 - 3,71 m depending on variant |
| Rotors | ||
| Main rotor diameter (m) |
1.2
12.8
62
|
|
| Tail rotor diameter (m) |
0.8
2.1
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
2,058
276,800
|
2066 - 2312 kg |
| Max. takeoff weight (Gross weight) (kg) |
154
3,742
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
289
28,165
|
|
| Сruise Speed (km/h) |
52
259
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
714
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
1,360
60,000
|
2 powerplants 618-700hp each depending on variant |
| Performance | ||
| Service ceiling (m) |
0.6
4,815
161,544
|
3901 0 4815 m depending on variant |
| Static ceiling (m) |
3
2,165
5,485
|
|
| Range (Ferry range) (km) |
4
900
40,700
|
600 - 900 km depending on variant |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
512
36,000
|
|
| Stat | ||
| Number built (qt) |
0
222
43,000
|
|
| Introduction | 1976 | |
| First flight | 13.08.1976 | |
