1. Czech Republic [1993-]
  2. Aircraft
  3. L-39NG

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 2027 Year Decommissioned 0
Agility 2.5 Damage Points (DP) 5
Empty Weight 3100 kg Max Weight 6300 kg
Runway Information 451-900m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 1450 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
Generic Night Vision Goggles LLTV, Night Vision Goggles (NVG) 0.00 - 15.00 nm 10 sec LLTV, 2nd Generation (1980s/1990s)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Night Vision Goggles SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 是

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 2.23 nm 4.88 nm 2.23 nm
Visual Classification Range 1.29 nm 2.87 nm 2.04 nm
Infrared Detection Range 2.23 nm 6.8 nm 11.71 nm
Infrared Classification Range 1.29 nm 2.87 nm 1.29 nm
Radar, A-D Band (30-2000 MHz) 3.2 dBsm (2.09 m²) 5.6 dBsm (3.63 m²) 3.2 dBsm (2.09 m²)
Radar, E-M Band (2-100 GHz) 3.2 dBsm (2.09 m²) 5.6 dBsm (3.63 m²) 3.2 dBsm (2.09 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 FJ44-4M Turbofan 1 1724 - 0.75 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1450