1. United States
  2. Aircraft
  3. Gulfstream G-IV SP [C-20J]

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1992 Year Decommissioned 0
Agility 1 Damage Points (DP) 10
Empty Weight 16100 kg Max Weight 33800 kg
Runway Information 901-1400m TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 2610 kg Crew 2 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
No Data

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
No Data

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
Passenger   x 18
Passenger   x 8

Signatures

Type Front Side Rear
Visual Detection Range 7.22 nm 14.01 nm 7.22 nm
Visual Classification Range 2.94 nm 5.9 nm 5.29 nm
Infrared Detection Range 4.81 nm 10.48 nm 15.79 nm
Infrared Classification Range 2.45 nm 4.92 nm 2.45 nm
Radar, A-D Band (30-2000 MHz) 12.4 dBsm (17.38 m²) 14.5 dBsm (28.18 m²) 12.4 dBsm (17.38 m²)
Radar, E-M Band (2-100 GHz) 12.4 dBsm (17.38 m²) 14.5 dBsm (28.18 m²) 12.4 dBsm (17.38 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/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
2x Rolls-Royce Tay 611-8 Turbofan 2 6288 - 0.4 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 13400