Basic Information

Category Helicopter Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 2020 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 940 kg Max Weight 1430 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size UAS [NATO Class II] (150-600kg)
Cost 0 Hypothetical No
Payload Weight 272 kg Crew 0 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation/Attack (Incl. Bomb, Rocket Delivery)

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/AAQ-22D BRITE Star II [IR/EO/Laser] Sensor Turret 0.00 - 0.00 nm 0 sec None

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/AAQ-22D BRITE Star II [IR/EO/Laser] SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 0.93 nm 2.8 nm 0.93 nm
Visual Classification Range 0.58 nm 1.67 nm 0.81 nm
Infrared Detection Range 1.04 nm 5.04 nm 8.7 nm
Infrared Classification Range 0.68 nm 1.97 nm 0.68 nm
Radar, A-D Band (30-2000 MHz) -9.1 dBsm (0.1230 m²) -6.3 dBsm (0.2344 m²) -9.1 dBsm (0.1230 m²)
Radar, E-M Band (2-100 GHz) -12.1 dBsm (0.0617 m²) -9.3 dBsm (0.1175 m²) -12.1 dBsm (0.0617 m²)

Default Configuration

Model Comments

Datalink

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

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x Rolls-Royce 250-C20W Helo Turboshaft 1 420 - 0.65 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 150