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 |