1. Tunisia
  2. Aircraft
  3. C-130J-30 Hercules

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 2013 Year Decommissioned 0
Agility 1 Damage Points (DP) 20
Empty Weight 34200 kg Max Weight 79200 kg
Runway Information 451-900m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 20000 kg Crew 5 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APN-242 Radar, Weather and Navigation 0.10 - 50.00 nm 2 sec Early 2000s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APN-242 SB1, SB2, SMF1, PB1, PB2, PMF2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Paratrooper   x 92
Trooper   x 128

Signatures

Type Front Side Rear
Visual Detection Range 6.46 nm 11.02 nm 6.46 nm
Visual Classification Range 3.13 nm 5.65 nm 5.92 nm
Infrared Detection Range 6.46 nm 11.7 nm 17.71 nm
Infrared Classification Range 3.13 nm 5.65 nm 3.13 nm
Radar, A-D Band (30-2000 MHz) 16 dBsm (39.81 m²) 17.9 dBsm (61.66 m²) 16 dBsm (39.81 m²)
Radar, E-M Band (2-100 GHz) 16 dBsm (39.81 m²) 17.9 dBsm (61.66 m²) 16 dBsm (39.81 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Unsecure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
4x AE 2100D3 Turboprop 4 6000 - 0.441 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 29300