Basic Information

Category Fixed Wing Type Trainer
Year Commissioned 1995 Year Decommissioned 2005
Agility 1.5 Damage Points (DP) 3
Empty Weight 3795 kg Max Weight 6835 kg
Runway Information 451-900m TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 2 people

Aircraft Capabilities

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic Comms Jammer Communications Jammer 0.00 - 0.00 nm 0 sec Early 2000s
Generic OECM [Average] OECM, Offensive ECM 0.00 - 0.00 nm 0 sec Early 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Comms Jammer SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2
Generic OECM [Average] 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 2.4 nm 4.43 nm 2.4 nm
Visual Classification Range 1.37 nm 2.64 nm 2.2 nm
Infrared Detection Range 2.4 nm 6.37 nm 12.06 nm
Infrared Classification Range 1.37 nm 2.64 nm 1.37 nm
Radar, A-D Band (30-2000 MHz) 4.1 dBsm (2.57 m²) 6.4 dBsm (4.37 m²) 4.1 dBsm (2.57 m²)
Radar, E-M Band (2-100 GHz) 4.1 dBsm (2.57 m²) 6.4 dBsm (4.37 m²) 4.1 dBsm (2.57 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
1x J33-A-35 Turbojet 1 2451 5400 1.14 2 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 2460