| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.7
88.7
|
|
| Height (m) |
0.6
3.6
50.1
|
|
| Rotors | ||
| Main rotor diameter (m) |
1.2
10.7
62
|
|
| Tail rotor diameter (m) |
0.8
1.7
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
1,210.2
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
2,721.6
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Useful load (kg) |
26.4
1,200
90,700
|
|
| Payload (kg) |
23
1,200
122,470
|
|
| Capacity passengers (per.) |
1
5
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
260
28,165
|
|
| Сruise Speed (km/h) |
52
246
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
556
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
812.3
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
5,696.7
161,544
|
|
| Static ceiling (m) |
3
3,718
5,485
|
|
| Range (Ferry range) (km) |
4
600.1
40,700
|
|
| Endurance (h) |
0.0
4.2
150
|
|
| Stat | ||
| Number built (qt) |
0
1,082
43,000
|
|
| Price (USD) |
41.5
2.5 million
750.0 million
|
|
| Introduction | 1994 | |
| First flight | 29.06.1995 | |
