1. China
  2. Aircraft
  3. Z-9W Haitun

Basic Information

Category Helicopter Type Attack
Year Commissioned 1990 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 2240 kg Max Weight 4250 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 1600 kg Crew 2 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation

Sensor Coverage Diagram
Model Detection Angle Omnidirectional

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
HJ-8A/C ATGM   x 4
HJ-8A/C ATGM   x 4
57mm Rocket   x 72
90mm Rocket   x 28
TY-90   x 4
TY-90   x 4

Signatures

Type Front Side Rear
Visual Detection Range 1.54 nm 4.51 nm 1.54 nm
Visual Classification Range 0.81 nm 2.28 nm 1.2 nm
Infrared Detection Range 1.54 nm 6.45 nm 10.15 nm
Infrared Classification Range 0.95 nm 2.68 nm 0.95 nm
Radar, A-D Band (30-2000 MHz) -1.3 dBsm (0.7413 m²) 1.3 dBsm (1.35 m²) -1.3 dBsm (0.7413 m²)
Radar, E-M Band (2-100 GHz) -1.3 dBsm (0.7413 m²) 1.3 dBsm (1.35 m²) -1.3 dBsm (0.7413 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Secure] 100 nm 0
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Secure] 300 nm 10
Radio HF Radio [Unsecure] 300 nm 10
HOT Weapon Link HJ-8 Command Wire 10 nm 1

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x WZ-8A [Arriel 1C1 Copy] Helo Turboshaft 2 700 - 0.55 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 900