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 |