| 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 | |
