| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
9.6
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Rotors | ||
| Disc area (m2) |
1.4
100.8
460
|
|
| Main rotor diameter (m) |
1.2
11.3
62
|
|
| Tail rotor diameter (m) |
0.8
1.8
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
858.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,338.1
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
1
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
169
28,165
|
|
| Сruise Speed (km/h) |
52
143
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
216
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
280
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
3,415
161,544
|
|
| Static ceiling (m) |
3
2,345
5,485
|
|
| Range (Ferry range) (km) |
4
396.3
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
262.1
36,000
|
|
| Stat | ||
| Number built (qt) |
0
5,600
43,000
|
|
| Introduction | 1960 | |
| First flight | 08.12.1945 | |
