| Technical, operational controls | AH-85A
|
| Crew | 1
|
| specifications |
|
| length | 11.84 m
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| width | m
|
| height | 3.47 m
|
| Main rotor diameter | 10.16 m
|
| diameter tail rotor | 1.57 mm
|
| empty weight | 820 kg
|
| maximum takeoff weight | 1450 kg
|
| maximum power 420 hp engine
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| Performance Specifications |
|
| ceiling hovering helicopter (IGE) | 3350 m
|
| ceiling hovering helicopter (OGE) | 2040 meters
|
| Service ceiling | 4160 m
|
| maximum rate of climb | 6.7 m s
|
| largest speed | 225 km per hour
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| range (5000 ft) | 875 km
|
| endurance | 5 hours
|
| applications |
ability to engage closely with fire performance of
high-speed flight at low altitude
search and goal-seeking
combat identification
|
| features |
body and blade and advanced composite materials
function in diverse geographical conditions
ability to perform different missions
high-performance
|
| Main variants |
AH-85A: Light overland version. It is intended for low-intensity policing conflicts or border patrol. Armed with a 7.62 mm machine-gun in the nose and two 70-mm rocket pods on hard-points.
AH-85B: Heavy overland version. Although it has yet to be seen, this model is said to be intended for "non-symmetrical wars". Nothing further is known.
AH-85C: Naval attack version. Equipped with a basic surface-search radar in it's nose instead of a machine-gun. Also equipped with a slightly different cockpit configuration then the AH-85A. Armament includes either two Kowsar AShMs or eight Sadid-1 missiles.
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