Basic Information

Category Fixed Wing Type Trainer
Year Commissioned 1980 Year Decommissioned 2005
Agility 3 Damage Points (DP) 5
Empty Weight 5350 kg Max Weight 9661 kg
Runway Information 451-900m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 2 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation
Jay Bird [RP-22 Sapfir-21] Radar, FCR, Air-to-Air, Short-Range 0.20 - 16.00 nm 2 sec Late 1960s
SPO-1 Sirena-1 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1950s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Jay Bird [RP-22 Sapfir-21] SB1, PB2
SPO-1 Sirena-1 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 2.21 nm 5.24 nm 2.21 nm
Visual Classification Range 1.28 nm 3.04 nm 2.02 nm
Infrared Detection Range 2.21 nm 7.13 nm 11.67 nm
Infrared Classification Range 1.28 nm 3.04 nm 1.28 nm
Radar, A-D Band (30-2000 MHz) 3 dBsm (2.00 m²) 5.4 dBsm (3.47 m²) 3 dBsm (2.00 m²)
Radar, E-M Band (2-100 GHz) 3 dBsm (2.00 m²) 5.4 dBsm (3.47 m²) 3 dBsm (2.00 m²)

Default Configuration

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

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 R-13F-300 Turbojet 1 4070 6495 0.95 2.25 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 2120