1. United States
  2. Aircraft
  3. C-141A Starlifter

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1966 Year Decommissioned 1981
Agility 1 Damage Points (DP) 20
Empty Weight 65542 kg Max Weight 146555 kg
Runway Information 1401-2000m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 28400 kg Crew 6 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APS-133 Radar, Weather and Navigation 0.50 - 300.00 nm 5 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APS-133 SB1, SB2, SMF1, PB1, PB2, PMF2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Paratrooper   x 120
Trooper   x 154

Signatures

Type Front Side Rear
Visual Detection Range 8.32 nm 14.45 nm 8.32 nm
Visual Classification Range 3.28 nm 6.02 nm 6.48 nm
Infrared Detection Range 8.32 nm 14.02 nm 19.54 nm
Infrared Classification Range 3.86 nm 7.08 nm 3.86 nm
Radar, A-D Band (30-2000 MHz) 19 dBsm (79.43 m²) 20.8 dBsm (120.23 m²) 19 dBsm (79.43 m²)
Radar, E-M Band (2-100 GHz) 19 dBsm (79.43 m²) 20.8 dBsm (120.23 m²) 19 dBsm (79.43 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio HF Radio [Secure] 300 nm 10
Radio AN/ARC-186(V) VHF Communications 100 nm 0
Radio AN/ARC-164 Have Quick II UHF Communications 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
4x TF33-PW-7 Turbojet 4 9534 - 0.56 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 68040