Basic Information

Category Fixed Wing Type Fighter
Year Commissioned 1965 Year Decommissioned 1990
Agility 2 Damage Points (DP) 10
Empty Weight 9970 kg Max Weight 17845 kg
Runway Information 1401-2000m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 3000 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
Skip Spin [RP-11 Oryol] Radar, FCR, Air-to-Air, Short-Range 0.10 - 35.00 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
Skip Spin [RP-11 Oryol] 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 3.2 nm 6.93 nm 3.2 nm
Visual Classification Range 1.74 nm 3.84 nm 2.94 nm
Infrared Detection Range 3.2 nm 8.59 nm 13.48 nm
Infrared Classification Range 1.74 nm 3.84 nm 1.74 nm
Radar, A-D Band (30-2000 MHz) 7.5 dBsm (5.62 m²) 9.8 dBsm (9.55 m²) 7.5 dBsm (5.62 m²)
Radar, E-M Band (2-100 GHz) 7.5 dBsm (5.62 m²) 9.8 dBsm (9.55 m²) 7.5 dBsm (5.62 m²)

Default Configuration

Model Comments

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-11AF2-300 Turbojet 2 3901 5752 0.941 2.206 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 5450