1. United Kingdom
  2. Aircraft
  3. Chinook HC.1 [CH-47C]

Basic Information

Category Helicopter Type Transport
Year Commissioned 1981 Year Decommissioned 1995
Agility 1 Damage Points (DP) 5
Empty Weight 10615 kg Max Weight 20865 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 6810 kg Crew 3 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation

Sensor Coverage Diagram
Model Detection Angle Omnidirectional

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Marine Infantry   x 48
Trooper   x 55
Trooper   x 33
Marine Infantry   x 24

Signatures

Type Front Side Rear
Visual Detection Range 2.06 nm 6.14 nm 2.06 nm
Visual Classification Range 1.21 nm 3.47 nm 1.89 nm
Infrared Detection Range 2.06 nm 7.92 nm 11.35 nm
Infrared Classification Range 1.21 nm 3.47 nm 1.21 nm
Radar, A-D Band (30-2000 MHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)
Radar, E-M Band (2-100 GHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio VHF Radio [Unsecure] 100 nm 0
Radio UHF 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 T55-L-11E Helo Turboshaft 2 3750 - 0.55 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 3130