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 |