Basic Information

Category Fixed Wing Type Fighter
Year Commissioned 1992 Year Decommissioned 1998
Agility 3 Damage Points (DP) 5
Empty Weight 10215 kg Max Weight 16520 kg
Runway Information 451-900m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical Yes
Payload Weight 2000 kg Crew 1 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
SPO-15L Beryoza RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1970s
IRST [TP-26] IRST, Non-Imaging Infrared Search and Track 0.00 - 40.00 nm 10 sec Infrared, Non-Imaging
High Lark 2 [Sapfir-23PA] Radar, FCR, Air-to-Air, Short-Range 0.20 - 40.00 nm 2 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
SPO-15L Beryoza SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
IRST [TP-26] SB1, PB2
High Lark 2 [Sapfir-23PA] SB1, PB2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 3.06 nm 6.06 nm 3.06 nm
Visual Classification Range 1.68 nm 3.43 nm 2.8 nm
Infrared Detection Range 3.06 nm 7.86 nm 13.25 nm
Infrared Classification Range 1.68 nm 3.43 nm 1.68 nm
Radar, A-D Band (30-2000 MHz) 7 dBsm (5.01 m²) 9.2 dBsm (8.32 m²) 7 dBsm (5.01 m²)
Radar, E-M Band (2-100 GHz) 7 dBsm (5.01 m²) 9.2 dBsm (8.32 m²) 7 dBsm (5.01 m²)

Default Configuration

Model Comments
23mm Gsh-23L [200 rnds] Aircraft, MiG-21, MiG-23

Datalink

Type Model Range Channels
Radio UHF 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 R-35-300 Turbojet 1 8565 13001 0.961 1.961 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 3600