Basic Information

Category Fixed Wing Type Fighter
Year Commissioned 1979 Year Decommissioned 1991
Agility 3 Damage Points (DP) 10
Empty Weight 10760 kg Max Weight 17900 kg
Runway Information 1401-2000m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 1500 kg Crew 1 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
Twin Scan [RP-26M Taifun-M2] Radar, FCR, Air-to-Air, Short-Range 0.10 - 35.00 nm 2 sec Late 1960s
SPO-3 Sirena-3 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Early 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Twin Scan [RP-26M Taifun-M2] SB1, PB2
SPO-3 Sirena-3 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 2.91 nm 6.82 nm 2.91 nm
Visual Classification Range 1.61 nm 3.79 nm 2.66 nm
Infrared Detection Range 2.91 nm 8.5 nm 12.98 nm
Infrared Classification Range 1.61 nm 3.79 nm 1.61 nm
Radar, A-D Band (30-2000 MHz) 6.4 dBsm (4.37 m²) 8.6 dBsm (7.24 m²) 6.4 dBsm (4.37 m²)
Radar, E-M Band (2-100 GHz) 6.4 dBsm (4.37 m²) 8.6 dBsm (7.24 m²) 6.4 dBsm (4.37 m²)

Default Configuration

Model Comments
23mm Gsh-6-23 [250 rnds] Aircraft, Su-15

Datalink

Type Model Range Channels
Radio UHF 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 R-13F2-300 Turbojet 2 4100 7050 0.95 2.25 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 5490