1. United States
  2. Aircraft
  3. F-4D Phantom II

Basic Information

Category Fixed Wing Type Multirole (Fighter/Attack)
Year Commissioned 1988 Year Decommissioned 1991
Agility 3 Damage Points (DP) 10
Empty Weight 13245 kg Max Weight 27500 kg
Runway Information 901-1400m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 8000 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APQ-109 Radar, FCR, Air-to-Air & Air-to-Surface, Medium-Range 0.30 - 60.00 nm 2 sec Early 1960s
AN/APS-107 STARM Target Acquisition Emitter Locator (For ARM Missiles) 0.00 - 120.00 nm 5 sec Late 1960s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APQ-109 SB1, PB2 否
AN/APS-107 STARM Target Acquisition 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 3.09 nm 6.77 nm 3.09 nm
Visual Classification Range 1.69 nm 3.76 nm 2.83 nm
Infrared Detection Range 3.09 nm 8.46 nm 13.29 nm
Infrared Classification Range 1.69 nm 3.76 nm 1.69 nm
Radar, A-D Band (30-2000 MHz) 7.1 dBsm (5.13 m²) 9.3 dBsm (8.51 m²) 7.1 dBsm (5.13 m²)
Radar, E-M Band (2-100 GHz) 7.1 dBsm (5.13 m²) 9.3 dBsm (8.51 m²) 7.1 dBsm (5.13 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
2x J79-GE-15 Turbojet 2 4944 7711 0.86 1.95 No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 5315