Basic Information

Category Fixed Wing Type Fighter
Year Commissioned 1979 Year Decommissioned 0
Agility 3.5 Damage Points (DP) 10
Empty Weight 13245 kg Max Weight 28000 kg
Runway Information 901-1400m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 8480 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/AWG-11 Radar, FCR, Air-to-Air & Air-to-Surface, Medium-Range 0.30 - 60.00 nm 2 sec Late 1960s
ARI.18228 [Sky Guardian] RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/AWG-11 SB1, PB2
ARI.18228 [Sky Guardian] 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 3.09 nm 6.77 nm 3.09 nm
Visual Classification Range 1.69 nm 3.76 nm 2.83 nm
Infrared Detection Range 3.09 nm 8.46 nm 13.29 nm
Infrared Classification Range 1.69 nm 3.76 nm 1.69 nm
Radar, A-D Band (30-2000 MHz) 7.1 dBsm (5.13 m²) 9.3 dBsm (8.51 m²) 7.1 dBsm (5.13 m²)
Radar, E-M Band (2-100 GHz) 7.1 dBsm (5.13 m²) 9.3 dBsm (8.51 m²) 7.1 dBsm (5.13 m²)

Default Configuration

Model Comments

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 Spey RB.168-25R RSp.2 Mk.202/Mk.203 Turbojet 2 5561 9313 0.86 1.95 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 5315