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 |