1. United States
  2. Aircraft
  3. AH-1S Cobra

Basic Information

Category Helicopter Type Attack
Year Commissioned 1981 Year Decommissioned 0
Agility 2 Damage Points (DP) 5
Empty Weight 2630 kg Max Weight 4535 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 2 people

Aircraft Capabilities

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

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

Signatures

Type Front Side Rear
Visual Detection Range 1.79 nm 5.19 nm 1.79 nm
Visual Classification Range 1.08 nm 3.01 nm 1.64 nm
Infrared Detection Range 1.79 nm 7.08 nm 10.76 nm
Infrared Classification Range 1.08 nm 3.01 nm 1.08 nm
Radar, A-D Band (30-2000 MHz) 0.5 dBsm (1.12 m²) 3 dBsm (2.00 m²) 0.5 dBsm (1.12 m²)
Radar, E-M Band (2-100 GHz) 0.5 dBsm (1.12 m²) 3 dBsm (2.00 m²) 0.5 dBsm (1.12 m²)

Default Configuration

Model Comments
M97 Turret [1x M197 20mm Cannon] AH-1E+

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Secure] 100 nm 0
TOW Weapon Link TOW Guidance Unit 20 nm 1

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x T53-L-703 Helo Turboshaft 1 1800 - 0.568 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 780