1. Civilian
  2. Aircraft
  3. H.135 T2

Basic Information

Category Helicopter Type Civilian
Year Commissioned 2002 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 1455 kg Max Weight 2910 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 1455 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
No Data

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
No Data

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
Passenger   x 6
No Data

Signatures

Type Front Side Rear
Visual Detection Range 2.17 nm 6.06 nm 2.17 nm
Visual Classification Range 1.08 nm 2.94 nm 1.59 nm
Infrared Detection Range 1.45 nm 6 nm 9.9 nm
Infrared Classification Range 0.9 nm 2.45 nm 0.9 nm
Radar, A-D Band (30-2000 MHz) -2.1 dBsm (0.6166 m²) 0.5 dBsm (1.12 m²) -2.1 dBsm (0.6166 m²)
Radar, E-M Band (2-100 GHz) -2.1 dBsm (0.6166 m²) 0.5 dBsm (1.12 m²) -2.1 dBsm (0.6166 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x Arrius 2B2 Helo Turboshaft 1 738 - 0.55 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 730