| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.9
88.7
|
fuselage only |
| Height (m) |
0.6
4.4
50.1
|
rotors folded |
| Width (m) |
1.9
3.5
7.7
|
|
| Rotors | ||
| Disc area (m2) |
1.4
387.4
460
|
|
| Main rotor diameter (m) |
1.2
15.7
62
|
|
| Weights | ||
| Loaded weight (kg) |
5
12,020.2
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
4
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
185.1
28,165
|
|
| Сruise Speed (km/h) |
52
154.5
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
2,400
60,000
|
1 powerplant |
| Performance | ||
| Range (Ferry range) (km) |
4
563
40,700
|
|
| Stat | ||
| Number built (qt) |
0
53
43,000
|
|
| Introduction | 1953 | |
| First flight | 03.03.1953 | |
