1. United States
  2. Aircraft
  3. CH-47C Chinook

Basic Information

Category Helicopter Type Transport
Year Commissioned 1969 Year Decommissioned 1990
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
AN/APR-39(V)1 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1960s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APR-39(V)1 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
Trooper   x 55
Trooper   x 33

Signatures

Type Front Side Rear
Visual Detection Range 2 nm 6.01 nm 2 nm
Visual Classification Range 1.18 nm 3.41 nm 1.83 nm
Infrared Detection Range 2 nm 7.81 nm 11.23 nm
Infrared Classification Range 1.18 nm 3.41 nm 1.18 nm
Radar, A-D Band (30-2000 MHz) 1.9 dBsm (1.55 m²) 4.3 dBsm (2.69 m²) 1.9 dBsm (1.55 m²)
Radar, E-M Band (2-100 GHz) 1.9 dBsm (1.55 m²) 4.3 dBsm (2.69 m²) 1.9 dBsm (1.55 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-11C Helo Turboshaft 2 3500 - 0.55 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 3130