Type | Helicopter | |
Company | Lockheed Corporation | |
Geometry | ||
---|---|---|
Length (m) |
1.9
16.7
88.7
|
|
Height (m) |
0.6
4.2
50.1
|
|
Rotors | ||
Main rotor diameter (m) |
1.2
15.6
62
|
|
Weights | ||
Empty weight (kg) |
8
5,540.6
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
11,739.0
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
one pilot, one copilot/gunner |
Hardpoints (qt) |
1
6
2,576
|
|
Speeds | ||
Max. Speed (km/h) |
25
393
28,165
|
|
Power | ||
Total Power (hp) |
0.4
3,927.6
60,000
|
|
Performance | ||
Service ceiling (m) |
0.6
6,100
161,544
|
|
Range (Ferry range) (km) |
4
1,971
40,700
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
914.4
36,000
|
|
Propellers | ||
Prop blade number (qt) |
1
4
8
|
on main rotor |
1
4
8
|
on tail rotor | |
1
3
8
|
on pusher propeller | |
Combat | ||
Guns (qt) |
1
2
18
|
nose turret with either an M129 40 mm (1.57 in) grenade launcher or an XM196 7.62x51 mm machine gun and belly turret with an XM140 30 mm (1.18 in) cannon |
Missiles (qt) |
1
-1
24
|
several 2.75 in (70 mm) FFA rockets |
Rockets (qt) |
1
-1
76
|
several BGM-71 TOW missiles |
Stat | ||
Number built (qt) |
0
10
43,000
|
|
Introduction | 1967 | |
First flight | 21.09.1967 |