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 |