Basic Information

Category Fixed Wing Type Fighter
Year Commissioned 1971 Year Decommissioned 1982
Agility 3 Damage Points (DP) 10
Empty Weight 12925 kg Max Weight 23770 kg
Runway Information 901-1400m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 1485 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
MG-13 Radar, FCR, Air-to-Air & Air-to-Surface, Short-Range 0.30 - 30.00 nm 2 sec Late 1950s
AN/APR-26 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1960s
Generic IRST IRST, Non-Imaging Infrared Search and Track 0.00 - 30.00 nm 10 sec Infrared, Non-Imaging

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
MG-13 SB1, PB2
AN/APR-26 SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
Generic IRST SB1, PB2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 3.24 nm 7.23 nm 3.24 nm
Visual Classification Range 1.76 nm 3.97 nm 2.97 nm
Infrared Detection Range 3.24 nm 8.84 nm 13.55 nm
Infrared Classification Range 1.76 nm 3.97 nm 1.76 nm
Radar, A-D Band (30-2000 MHz) 7.7 dBsm (5.89 m²) 9.9 dBsm (9.77 m²) 7.7 dBsm (5.89 m²)
Radar, E-M Band (2-100 GHz) 7.7 dBsm (5.89 m²) 9.9 dBsm (9.77 m²) 7.7 dBsm (5.89 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 J57-P-55 Turbojet 2 5443 7711 0.785 1.95 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 6215