| Type | Helicopter | |
| Company | Bell Aircraft Corporation | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.1
88.7
|
with both rotors turning |
| Height (m) |
0.6
4.1
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
44
95
|
|
| Rotors | ||
| Main rotor diameter (m) |
1.2
13.4
62
|
|
| Tail rotor diameter (m) |
0.8
2.6
4.9
|
|
| Weights | ||
| Empty weight (kg) |
8
2,993.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
4,535.9
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
one pilot, one co-pilot/gunner |
| Speeds | ||
| Max. Speed (km/h) |
25
277
28,165
|
|
| Never exceed speed (km/h) |
108.0
315
1,050
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
980
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
1,800
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
3,718.6
161,544
|
|
| Range (Ferry range) (km) |
4
507.5
40,700
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
493.8
36,000
|
|
| Combat | ||
| Guns (qt) |
1
1
18
|
General Dynamics 20 mm (0.787 in) M197 3-barreled Gatling cannon |
| Missiles (qt) |
1
8
24
|
missiles mounted in two-missile launchers on each hardpoint |
| Rockets (qt) |
1
7
76
|
mounted in the M260 launcher |
| Stat | ||
| Number built (qt) |
0
1,116
43,000
|
|
| Price (USD) |
41.5
11.3 million
750.0 million
|
|
| Introduction | 1967 | |
| First flight | 07.09.1965 | |
