1. United States
  2. Aircraft
  3. KC-130F Hercules

Basic Information

Category Fixed Wing Type Tanker (Air Refueling)
Year Commissioned 1962 Year Decommissioned 2006
Agility 1 Damage Points (DP) 20
Empty Weight 30040 kg Max Weight 61235 kg
Runway Information 901-1400m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 21165 kg Crew 7 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APN-59 Radar, Weather and Navigation 0.50 - 40.00 nm 2 sec Early 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APN-59 SB1, SB2, SMF1, PB1, PB2, PMF2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 9.69 nm 16.48 nm 9.69 nm
Visual Classification Range 3.76 nm 6.76 nm 7.11 nm
Infrared Detection Range 6.46 nm 11.68 nm 17.71 nm
Infrared Classification Range 3.13 nm 5.64 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
No Data

Datalink

Type Model Range Channels
Radio AN/ARC-52 UHF Communications 50 nm 0
Radio AN/ARC-34 UHF Communications 100 nm 0
Radio AN/ARC-38 HF Communications 100 nm 0
Radio AN/ARC-38A HF Communications 100 nm 0
Radio AN/ARC-94 HF Communications 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
4x Allison T56-A-7 Turboprop 4 4300 - 0.54 - No Allison T56-A-16(?)

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 32340