Type | Helicopter | |
Company | Bell Aircraft Corporation | |
Geometry | ||
---|---|---|
Length (m) |
1.9
12.9
88.7
|
|
Height (m) |
0.6
3.9
50.1
|
|
Rotors | ||
Disc area (m2) |
1.4
1.4
460
|
|
Main rotor diameter (m) |
1.2
10.7
62
|
|
Tail rotor diameter (m) |
0.8
1.7
4.9
|
|
Weights | ||
Empty weight (kg) |
8
1,586
276,800
|
|
Loaded weight (kg) |
5
2,495
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
240
28,165
|
|
Сruise Speed (km/h) |
52
176
3,087
|
|
Fuel | ||
Fuel Capacity (l) |
23
454
320,000
|
|
Power | ||
Total Power (hp) |
0.4
650
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
4,575
161,544
|
|
Static ceiling (m) |
3
3,660
5,485
|
|
Range (Ferry range) (km) |
4
260
40,700
|
|
Endurance (h) |
0.0
2
150
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
492
36,000
|
|
Combat | ||
Guns (qt) |
1
1
18
|
M3P .50 cal (12.7mm) machine gun |
Missiles (qt) |
1
4
24
|
2 x AGM-114 Hellfire missiles and 2 x JAGM (Joint Air-to-Ground Missile) |
Rockets weight (kg) |
1
1
48
|
M260 rocket launcher w/ seven 2.75" Hydra 70 rockets |
Stat | ||
Number built (qt) |
0
2,200
43,000
|
|
Price (USD) |
41.5
4.9 million
750.0 million
|
|
Introduction | 1983 | |
First flight | 10.01.1966 |