1. United States
  2. Aircraft
  3. CH-46E Sea Knight

Basic Information

Category Helicopter Type Transport
Year Commissioned 1979 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 6287 kg Max Weight 11000 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 3000 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)2 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1960s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APR-39(V)2 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
Marine Infantry   x 12
Marine Infantry   x 24

Signatures

Type Front Side Rear
Visual Detection Range 1.94 nm 5.44 nm 1.94 nm
Visual Classification Range 0.97 nm 2.67 nm 1.51 nm
Infrared Detection Range 1.94 nm 7.31 nm 11.09 nm
Infrared Classification Range 1.15 nm 3.14 nm 1.15 nm
Radar, A-D Band (30-2000 MHz) 1.5 dBsm (1.41 m²) 3.9 dBsm (2.45 m²) 1.5 dBsm (1.41 m²)
Radar, E-M Band (2-100 GHz) 1.5 dBsm (1.41 m²) 3.9 dBsm (2.45 m²) 1.5 dBsm (1.41 m²)

Default Configuration

Model Comments
12.7mm/72 GAU-15 MG [2400 rnds] -
12.7mm/72 GAU-15 MG [2400 rnds] -

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 T58-GE-16 Helo Turboshaft 2 1870 - 0.62 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1175