|
Developing Nation: |
Russia. |
|
Task: |
Two seat attack helicopter. |
|
First Flight: |
November 10, 1982. |
|
First Delivery: |
no production frames ordered. |
|
Crew: |
2.
- front cockpit for navigator
/ weapons operator.
- rear cockpit for pilot.
- A rear fuselage compartment
can hold two or three people, intended for emergency
recovery of personnel only. |
|
Main rotor
Span: |
17.20 m. |
|
Length: |
17.01 m (without rotors). |
|
Height: |
3.82 m to top of rotor head. |
|
Engine (s): |
Klimov TV3 turbo shafts driving a five blade main rotor and
four blade tail rotor 2x (2.465 hp each). |
|
Weight: |
8.590 kg. |
|
Max.Take off weight: |
11.500 kg. |
|
Max. Speed: |
320 km/h. |
|
Max. Range: |
- 460 km (with standard
fuel).
- 1.100 km (ferry range with
reserves).
- Endurance with max fuel
2hr. |
|
Weapons: |
- One NPPU-28 30 mm cannon in
under nose turret.
- four underwing hardpoints
can carry an ordnance load of 1.920 kg.
- typical configuration: two
rocket pods, and up to 16 9P149 Shturm C (AT-6 Spiral) radio
guided tube launched anti armor missiles |
