| 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 | |
