1. Israel
  2. Aircraft
  3. A-4N Skyhawk [Ahit]

Basic Information

Category Fixed Wing Type Attack
Year Commissioned 1982 Year Decommissioned 0
Agility 3 Damage Points (DP) 5
Empty Weight 4750 kg Max Weight 11136 kg
Runway Information 901-1400m TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 8318 kg Crew 1 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing Probe Refueling

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APG-53A Radar, FCR, Air-to-Air & Air-to-Surface, Short-Range 0.20 - 16.00 nm 2 sec Late 1960s
Generic RWR RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Late 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APG-53A SB1, PB2 否
Generic RWR 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 2.15 nm 4.9 nm 2.15 nm
Visual Classification Range 1.25 nm 2.87 nm 1.97 nm
Infrared Detection Range 2.15 nm 6.82 nm 11.55 nm
Infrared Classification Range 1.25 nm 2.87 nm 1.25 nm
Radar, A-D Band (30-2000 MHz) 2.7 dBsm (1.86 m²) 5.1 dBsm (3.24 m²) 2.7 dBsm (1.86 m²)
Radar, E-M Band (2-100 GHz) 2.7 dBsm (1.86 m²) 5.1 dBsm (3.24 m²) 2.7 dBsm (1.86 m²)

Default Configuration

Model Comments
30mm DEFA 552 x 2 [125 rnds x 2] Aircraft, Mirage III

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
1x J52-P-408 Turbojet 1 5084 - 0.79 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 2360