Basic Information

Category Fixed Wing Type Target Drone
Year Commissioned 1981 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 199 kg Max Weight 0 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 0 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic DECM [Average] DECM, Defensive ECM 0.00 - 0.00 nm 0 sec Early 1980s
AN/APS-130 Radar, Surface Search, Medium-Range 0.30 - 150.00 nm 4 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic DECM [Average] SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
AN/APS-130 SB1, SB2, SMF1, PB1, PB2, PMF2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 1.03 nm 2.32 nm 1.03 nm
Visual Classification Range 0.58 nm 1.32 nm 0.75 nm
Infrared Detection Range 0.69 nm 3.16 nm 7.4 nm
Infrared Classification Range 0.48 nm 1.1 nm 0.48 nm
Radar, A-D Band (30-2000 MHz) -11.1 dBsm (0.0776 m²) -8.1 dBsm (0.1549 m²) -11.1 dBsm (0.0776 m²)
Radar, E-M Band (2-100 GHz) -11.1 dBsm (0.0776 m²) -8.1 dBsm (0.1549 m²) -11.1 dBsm (0.0776 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
1x J400-WR-402/3 Turbofan 1 81 - 1.2 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 35